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Article

SORA 2.5-Guided BVLOS UAS for Wildlife Conservation in Kenya: Reducing Friction Between Safety and Field Operations

by
Guy Maalouf
1,*,
Thomas Stuart Richardson
2,
David Roy Guerin
3,
Matthew Watson
4,
Ulrik Pagh Schultz Lundquist
1,
Blair R. Costelloe
5,6,7,
Elzbieta Pastucha
1,
Saadia Afridi
1,8,
Edouard George Alain Rolland
1,
Kilian Meier
2,
Jes Hundevadt Jepsen
1,
Thomas van der Sterren
1,
Lucie Laporte-Devylder
9,
Camille Rondeau Saint-Jean
9,
Constanza Andrea Molina Catricheo
10,
Vandita Shukla
10,11,
Elena Iannino
5,6,
Jenna Kline
12,
Dat Nguyen Ngoc
13,
William Njoroge
14 and
Kjeld Jensen
1
add Show full author list remove Hide full author list
1
SDU UAS Center, University of Southern Denmark, 5230 Odense, Denmark
2
Bristol Flight Lab, University of Bristol, Bristol BS8 1QU, UK
3
Global Drone Forum, Brisbane 4051, Australia
4
School of Earth Sciences, University of Bristol, Bristol BS8 1QU, UK
5
Department of Collective Behavior, Max Planck Institute of Animal Behavior, 78464 Konstanz, Germany
6
Department of Biology, University of Konstanz, 78464 Konstanz, Germany
7
Centre for the Advanced Study of Collective Behaviour, University of Konstanz, 78464 Konstanz, Germany
8
Avy B.V., 1043 AJ Amsterdam, The Netherlands
9
Department of Biology, University of Southern Denmark, 5230 Odense, Denmark
10
Institute for Geoinformatics, University of Münster, 48149 Münster, Germany
11
3D Optical Metrology Unit (3DOM), Fondazione Bruno Kessler (FBK), 38123 Trento, Italy
12
Department of Computer Science and Engineering, The Ohio State University, Columbus, OH 43210, USA
13
School of Computer Science, University of Bristol, Bristol BS8 1QU, UK
14
Ol Pejeta Conservancy, Nanyuki 10400, Kenya
*
Author to whom correspondence should be addressed.
Drones 2026, 10(3), 178; https://doi.org/10.3390/drones10030178
Submission received: 2 December 2025 / Revised: 28 January 2026 / Accepted: 30 January 2026 / Published: 5 March 2026
(This article belongs to the Special Issue UAVs for Nature Conservation Tasks in Complex Environments)

Highlights

What are the main findings?
  • In conservation environments, ground risk is largely driven by transient populations (e.g., tourism and ranger activity), which are not reliably captured by standard population raster datasets.
  • Formal safety requirements and field realities are often misaligned in wildlife operations, creating operational friction between prescribed procedures and practical execution.
What are the implications of the main findings?
  • Ground-risk assessments in conservancies should prioritise bottom-up, activity-based population estimates, using raster products primarily for triangulation and sensitivity analysis.
  • Reducing friction between safety requirements and field needs, through iterative crew optimisation and mission-specific procedure design, can improve both operational efficiency and procedural compliance.

Abstract

Safe Beyond Visual Line of Sight (BVLOS) operations are increasingly required for wildlife monitoring and conservation, yet existing regulatory frameworks are rarely tailored to protected areas characterised by low population density and limited infrastructure. This paper presents a field-based use case illustrating how the Specific Operations Risk Assessment (SORA) methodology can be applied to conservation-oriented BVLOS missions under Kenyan airspace conditions, including coordination within military-controlled airspace. We evaluate three population-density estimation approaches (qualitative, bottom-up, and top-down) against available ground truth, and compare tabulated and analytical SORA methods for deriving the Ground Risk Class. The work illustrates how SORA 2.5 structures ground and air risk reasoning in a conservation context, while retrospective review identifies limitations in containment, Operational Safety Objectives, and tactical mitigation performance requirements. Field trials involved five concurrent teams and 30 personnel conducting over 260 flights and more than 60 h of UAS activity across the Ol Pejeta Conservancy, providing insights into multi-team coordination under field conditions. Field implementation revealed areas of misalignment between prescribed safety requirements and operational realities, prompting iterative adaptation of workflows and procedures. Observed outcomes included reductions in team size (25–50%) and procedural steps (18%), derived from retrospective comparison of field procedures. A lightweight Uncrewed Traffic Management prototype was also trialled, revealing practical limitations in conservancy environments. Finally, we present a ten-step framework for developing field-ready safety procedures to support risk-informed decision-making in non-standard operational contexts. The findings provide empirically grounded guidance on applying SORA principles to conservation UAS missions, without proposing a new risk framework or generalised operational model.

1. Introduction

Uncrewed Aerial System (UAS) have become an important tool for wildlife conservation by enabling high-resolution data collection across large or inaccessible areas with minimal disturbance to animals [1,2,3]. Their flexibility supports increasingly demanding applications, including Beyond Visual Line of Sight (BVLOS) and multi-UAS operations [4,5]. As such operations scale in range, duration, and coordination complexity, the primary challenge shifts from platform capability to ensuring missions are conducted safely within regulatory and operational constraints. Despite a growing body of literature on conservation UAS applications, few peer-reviewed studies document how established risk assessment frameworks [6] translate into field-ready procedures in remote conservation environments. Empirical evidence remains limited on how Specific Operations Risk Assessment (SORA)-derived requirements interact with transient population exposure, limited infrastructure, and non-standard airspace governance [7,8]. As a result, friction arising from applying risk-based frameworks in conservation campaigns remains under-reported.
The SORA provides a structured framework for assessing and mitigating risks in UAS operations [9,10,11], but its application in conservation settings is challenged by remote environments, limited infrastructure, and the need to adapt flight plans to animal movement and changing local conditions. As a result, ensuring that safety requirements remain compatible with research objectives requires field testing and context-specific adaptation [12]. Within this context, this study reports on 2025 field campaigns conducted at the Ol Pejeta Conservancy in Kenya (360 km2), building on earlier operations in 2024 [13] and extending them to multi-team BVLOS deployments involving multiple UAS, pilots, and lightweight coordination tools as part of the WildDrone project [14].

1.1. Kenyan Regulatory Context

The Kenyan Civilian Aviation Authority (KCAA)’s UAS Regulations 2020 [15] classify UAS operations into Categories A–C according to operational risk and complexity. BVLOS flights fall under Category C and require integration with Air Traffic Control (ATC) and compliance with the KCAA’s Rules of the Air, summarised in Appendix A.1.
At the time of writing, the KCAA did not issue standard BVLOS authorisations pending the establishment of a national Uncrewed Traffic Management (UTM). The reported operations were therefore conducted under a specific exemption within prohibited military airspace covering Ol Pejeta, subject to prior approval and real-time coordination with Kenyan Air Force (KAF) ATC. In the absence of formal separation standards between crewed and uncrewed aircraft, airspace safety relied on procedural coordination and radio communication. The operations required both a temporary import permit for each UAS and an operational permit for the BVLOS missions [16], facilitated through the local partner Kenya Flying Labs (KFL). Further regulatory definitions, permit requirements, and document templates are provided in Appendix A.2, and the full submission set is available in an open-access repository (https://github.com/GuyMaalouf/wilddrone-hackathon-2025-bvlos-ops, accesssed on 29 January 2026).

1.2. Study Aim

This study examines how SORA 2.5 can be applied to the planning and execution of BVLOS operations in protected conservation areas characterised by low population density and limited infrastructure, within a specific Kenyan regulatory context that includes coordination with military-controlled airspace. Drawing on field campaigns conducted in Kenya, the analysis evaluates how SORA 2.5 can be adapted to conservation environments and identifies sources of friction between formal safety requirements and the practical constraints of fieldwork. The study makes two main contributions: (i) an empirical assessment of how ground risk can be characterised in conservation areas, including the treatment of transient populations and the practical use of different intrinsic Ground Risk Class (iGRC) assessment approaches, and (ii) an analysis of how risk assessment outcomes can be translated into scalable, field-ready procedures for multi-team BVLOS operations supported by lightweight coordination tools. The aim is to provide empirically grounded insights into the practical application of SORA in non-standard operational contexts, rather than to propose a new risk framework.

1.3. Research Questions

The analysis is structured around four research questions:
  • RQ 1—How can SORA 2.5 guide the planning of BVLOS operations in conservation areas?
    • RQ 1.1: How can SORA 2.5 ground-risk approaches be used in conservation settings, and how do they compare in that context?
    • RQ 1.2: Which safety constraints affect conservation fieldwork, and how can they be addressed?
  • RQ 2—How should safety procedures be designed to meet the needs of conservation fieldwork?
    • RQ 2.1: How much efficiency can be gained by tailoring procedures to specific missions?
    • RQ 2.2: Which procedural elements can be automated, and how does automation affect crew workload and reliability?
  • RQ 3—How can BVLOS operations be scaled to multiple teams while preserving safety in the field?
    • RQ 3.1: How can crew configurations be optimised to improve scalability while maintaining safety, and what trade-offs arise?
  • RQ 4—What needs to happen for field-supported BVLOS operations to become fully remote?

1.4. Reading Guide

Readers seeking the main insights can begin with Section 5 (Discussion), which answers the research questions and synthesises regulatory, procedural, and operational findings. Section 2, Section 3 and Section 4 provide the supporting analysis: Section 2 outlines the SORA-guided risk assessment, including the comparison of population-density methods and tabulated versus analytical computation of intrinsic Ground Risk Class; Section 3 describes procedure design, crew coordination, and multi-team operations; Section 4 presents field results and recurring operational challenges. Appendix A summarises the Kenyan regulatory framework and permit process, Appendix B provides supplementary SORA calculations and definitions, and Appendix C contains mission-level field trial cards.

2. SORA 2.5-Based Risk Assessment in a Conservation Environment

SORA 2.5 was used as guidance to structure the risk assessment and safety planning for BVLOS operations under Kenyan airspace conditions. This section summarises how the relevant SORA steps informed the pre-operation classification of ground and air risk, and how the remaining elements of the framework were evaluated retrospectively following the January 2025 Ol Pejeta campaign, with detailed calculations, procedural artefacts, and extended analyses provided in the Appendix A, Appendix B and Appendix C to support, but not interrupt, the main narrative. Particular emphasis is placed on ground-risk assessment and the conservation-specific considerations affecting population-density estimation. Supplementary calculations and extended analyses, including post-operation evaluations of Operational Safety Objectives (OSOs), containment, and tactical-mitigation requirements, are provided in Appendix B. It is important to note that the SORA addresses only third-party ground and air risks; internal field-team safety considerations (such as wildlife encounters or heat exposure) fall outside its scope and were managed through separate operational protocols.

2.1. Step 1: Documentation of the Proposed Operation

What—Mission Objective: Conduct BVLOS flights to support wildlife conservation at Ol Pejeta, including ecological mapping, animal tracking, and environmental monitoring.
Where—Area of Operation: Flights took place within the 360 km2 fenced Ol Pejeta Conservancy in central Kenya, a sparsely populated wildlife reserve containing several lodges and camps relevant to ground-risk assessment. The area lies under KCAA jurisdiction within military-controlled airspace, requiring coordination with both civilian and military ATC.
Which—Platforms Used: A total of 14 UASs were used, combining Commercial Off-The-Shelf (COTS) and research platforms. COTS multirotors comprised DJI Mavic 3 variants (Enterprise, Thermal, Pro), DJI Mini 3, Parrot Anafi, and CoDrone systems (Aluco, Noctu). Research platforms included the “Papa Smurf” quadcopter developed by the University of Bristol. Two fixed-wing systems were deployed: the Ebee X and a solar-powered University of Bristol glider. This mix provided complementary endurance, range, and payload capabilities for the different conservation tasks undertaken.

2.2. Step 2: iGRC

Step 2 estimates the iGRC by assessing the population-density within the operational footprint. We first defined a top-down containment geometry, then applied three population-estimation methods (qualitative field knowledge, tourism-based bottom-up, and raster-based top-down) and mapped the resulting densities to iGRC using both the tabulated SORA 2.5 method and the analytical approach of SORA Annex F.

2.2.1. SORA Semantic Map and Top-Down Volume Definition

We constructed a semantic map for Ol Pejeta, seen in Figure 1, based on the SORA semantic volumes, more details available in Appendix B.1.
A top-down approach was adopted: starting from the fenced conservancy boundary, we defined a bounded risk footprint that excludes surrounding villages and marks campgrounds as no-fly zones. This configuration aligns the ground-risk footprint with the conservancy fence, simplifies regulatory justification, and helps keep both routine and failure scenarios contained within the conservancy. Buffer-sizing considerations and a comparison with a bottom-up, path-based alternative are provided in Appendix B.2.
Note on units: This paper uses metric, imperial, and nautical units according to operational convention. Altitudes and regulatory limits are expressed in feet to match KCAA practice, horizontal distances and buffer sizes are given in metres or kilometres following UAS specifications, and airspace separation distances use nautical miles where appropriate.

2.2.2. Qualitative Estimation Using Field Knowledge

The initial iGRC assessment followed the SORA Annex F guidelines using a qualitative estimate of the average population density within the iGRC footprint (flight geography + contingency + ground-risk buffer). This estimate drew on prior BVLOS campaigns at Ol Pejeta and input from rangers and conservancy management. Human presence inside the fenced conservancy consists primarily of resident staff and their families, concentrated around staff compounds, operational centres, and a small number of lodges. Tourist activity is similarly localised around camps and attractions, with additional transient movement during game drives. Because the conservancy is fenced and not accessible to surrounding communities, there is no casual or unregulated foot traffic from outside the reserve.
Taken together, this restricted and spatially clustered pattern of human activity, combined with the absence of dense settlements or large buildings within the risk footprint, supported classifying the area as “lightly populated” (<50 people/km2). Classification criteria and supporting evidence are summarised in Appendix B.3.

2.2.3. Tourism-Based Local Estimation (Bottom-Up Approach)

A bottom-up estimate of population exposure was derived by projecting 2025 tourist visits to Ol Pejeta from official conservancy statistics (2016–2022) and regional post-COVID recovery rates from UN Tourism [17,18], yielding approximately 116,800 visitors (Figure 2).
A low-season adjustment for January resulted in an average of 352 tourists per day. Assuming an even distribution across 10 active camps and adding 10 staff per camp produced an estimated 46 people/km2, corresponding to the “lightly populated” category. Intermediate values are summarised in Table 1, with derivations in Appendix B.4.

2.2.4. Population Raster Analysis (Top-Down Approach)

As a complementary top-down method, residential population within the conservancy was estimated using the 2020 WorldPop gridded dataset for Kenya [20]. Rasters were analysed at 100, 200, and 500 m resolutions to assess grid-size sensitivity (Figure 3).
A distribution derived from the 100 m grid (Figure 4) was used to characterise density variation across the operational area, yielding an average density of 12 people/km2 and a maximum of 105 people/km2. Aggregation to 200 m and 500 m reduced the maxima to 58 and 53 people/km2, respectively, illustrating how coarser grids smooth local peaks.
Because SORA relies on the maximum population density, the choice of raster resolution has a direct effect on iGRC classification. At 200 m and 500 m, WorldPop maxima were close to, but slightly above, the qualitative and tourism-based estimates (<50 people/km2), whereas the 100 m grid produced an isolated extreme value more than twice as high. Figure 4 shows this as a tail event, highlighting how fine-resolution rasters can introduce single-cell outliers that disproportionately influence SORA outcomes. As WorldPop represents residential, typically night-time population, it does not capture transient tourist or staff presence within the fenced conservancy. Processing steps are summarised in Appendix B.5, and the full analysis code is available on GitHub (https://github.com/GuyMaalouf/opc-worldpop-analysis, accessed on 29 January 2026).

2.2.5. Ground-Truth Validation of Population Estimates

To validate the population estimates, daily visitor records from Ol Pejeta Conservancy were used as time-bounded, post-campaign ground-truth data derived from administrative records rather than real-time tracking. The observed mean of 309 tourists/day closely matched the bottom-up estimate of 352 tourists/day, while a transient spike exceeding 550 visitors occurred on 31 January (Figure 5).
Visitor distribution across camps showed strong spatial clustering (Figure 6), with most camps hosting small groups of 5–15 guests/day and a clear outlier at Sweetwaters Tented Camp, which averaged 112 visitors/day and exceeded 200 visitors on one day.
Approximately 600 staff were present daily across multiple facilities. These observations confirm that the conservancy remains lightly populated on average, while revealing short-lived surges and localised hotspots that are not captured by static or coarse-resolution population models and that must be addressed through conservative planning assumptions within the SORA process.

2.2.6. Determination of iGRC Based on the SORA Table

To complete Step 2, we identified the iGRC using the tabulated method in the SORA 2.5 framework [9]. The population-density value used for the table lookup was the <50 people/km2 category, consistent with the qualitative and tourism-based methods described earlier. For the platform characteristics, we selected the University of Bristol solar-powered glider as the representative UAS because it had the largest wingspan and highest cruise speed among all platforms deployed. Its 3.8 m wingspan places it in the 3–8 m characteristic-dimension category, and its 20 m/s cruise speed falls within the <25 m/s category. Following the SORA requirement to use the higher-risk of the two, the 3–8 m column was selected.
The intersection of the <50 ppl/km2 row with the 3–8 m column results in iGRC 5. The complete table used for this classification is reproduced in Appendix B.6.

2.2.7. Refined iGRC Estimation Using Annex F

We then applied the analytical method in SORA Annex F, which replaces the stepwise table with a continuous risk metric using the critical area  A C and population density D pop . Using the same UAS parameters and density estimates, Annex F yielded iGRC 4, one class lower than the tabulated iGRC 5. Full calculations are provided in Appendix B.7.
This difference reflects the discrete structure of the tabulated method: the University of Bristol solar glider lies close to the boundary of the 3–8 m characteristic-dimension column, where small changes in wingspan or population estimates can produce relatively coarse shifts in the tabulated result. Annex F offers a finer-grained calculation in such edge cases, producing a slightly lower intrinsic ground-risk value.

2.3. Step 3: Final Ground Risk Class (GRC)

Starting from the refined iGRC 4 (SORA Annex F, Section 2.2.7), we applied exposure-reduction (M1) ground-risk mitigations from Annex B of SORA 2.5, implemented primarily through operational and procedural controls rather than additional onboard systems, to reduce exposure of uninvolved people (Table 2). No energy-reduction devices (M2) were available on the platforms.
According to the Annex B reduction scheme, the combination of M1a (low), M1b (medium), and M1c (low) is valid and yields a three-step reduction, lowering the ground-risk classification from iGRC 4 to a final GRC 1. Full details are provided in Appendix B.8.

2.4. Step 4: Initial Air Risk Class (iARC)

The initial Air Risk Class (iARC) reflects the expected encounter rate with crewed aircraft in the operational volume before applying strategic mitigations. All flights took place inside the military-controlled restricted area HKR10 (Nanyuki), which overlaps a prohibited zone (HKP2) frequently used by KAF. This resulted in a classification of iARC–c.
Although the conservancy itself is rural, low-flying crewed aircraft, primarily tourist and charter traffic, were regularly observed, and one overflight during daytime operations required the UAS to descend below 30 m Above Ground Level (AGL) and temporarily pause the mission. Night flights were conservatively assigned the same iARC–c category.

2.5. Step 5: Strategic Air-Risk Mitigations

Strategic mitigations were applied before take-off to reduce the likelihood of encounters with crewed aircraft in the restricted and prohibited airspace over Ol Pejeta. These measures, combined with coordination from KAF, reduced the initial classification from iARC–c to a residual ARC–b. The applied mitigations are listed in Table 3.
The residual assessment relied on procedural deconfliction established by KAF ATC, including a vertical buffer between UAS operations and the lowest crewed flight levels and direct coordination before each operation. These measures ensured consistent separation within a controlled airspace and justified reducing the initial iARC–c to ARC–b.

2.6. Step 6: Tactical Mitigation Performance Requirements

For ARC–b operations, we applied the low-robustness Tactical Mitigation Performance Requirements (TMPR) defined in SORA Annex D. Tactical mitigations primarily relied on observers, ATC information, and radio-based situational awareness rather than automated detect-and-avoid systems. The measures implemented during the January 2025 campaign covered detection, decision-making, command, execution, and feedback using the available systems.
While these measures satisfy the qualitative requirements for low-robustness TMPRs, the absence of independent ground-truth air traffic data over the conservancy prevented empirical verification of detection probability, which was therefore treated as a known limitation in the retrospective assessment. A concise summary is provided in Table 4, with an adapted overview of the Annex D requirements in Appendix B.9.

2.7. Step 7: Specific Assurance and Integrity Level (SAIL)

The final ground risk (GRC 1) and residual air risk (ARC-b) combine to give a Specific Assurance and Integrity Level (SAIL) II operation according to the SORA Step 7 matrix. This level determines the robustness levels of containment requirements and Operational Safety Objectives (OSOs) that must be addressed in subsequent steps. The full SAIL matrix and mapping are provided in Appendix B.11.

2.8. Step 8: Containment Requirements

Containment requirements were based on adjacent-area population density and the characteristic dimension of the largest platform (3.8 m wingspan). Raster analysis of the 5 km adjacent area (Appendix B.12) indicated densities of 45–50 ppl/km2, local maxima below 500 ppl/km2, and no large assemblies within 1 km of the operational boundary.
Using the SORA 2.5 tabulated method (SORA main body Table 11 [9]; Appendix B.13), the operation corresponds to a Low containment requirement because the UAS exceeds the 3 m characteristic-dimension category. For comparison, the analytical SORA Annex F method (§5.3) was applied. The refined calculation in Appendix B.14, using D p o p 50  people/km2, yielded i G R C adj = 4 . As shown in Appendix B.15, no ground-risk mitigations applied in the adjacent area, and Appendix B.16 reports the corresponding Annex F Table 27 [9] outcome of no containment requirement for a SAIL II operation.
Both methods indicate minimal population exposure outside the conservancy, with the Annex F analytical approach yielding a less conservative yet compliant result. This reflects the intended SORA 2.5 trade-off: the tabulated method provides a faster, conservative option, whereas the analytical method requires additional effort but offers a more representative assessment in non-standard environments such as wildlife conservancies.

2.9. Step 9: Operational Safety Objectives (OSOs)

Due to timeline constraints, a clause-by-clause OSO assessment was not performed before fieldwork; instead, operational safety was ensured through pre-defined procedures, training, and checklists. Following the campaign, the operation was retrospectively reviewed against SORA 2.5 Annex E requirements for a SAIL II mission to assess compliance.
The review showed that several OSOs were met, others were partially met (typically due to incomplete documentation such as maintenance records or the absence of an Emergency Response Plan), and one OSO was not met, with the identified gaps primarily reflecting limitations in organisational assurance and documentation maturity rather than deficiencies observed during in-field operations, thereby providing a structured basis for prioritising improvements in future campaigns. A summary of OSO compliance is provided in Table 5, with detailed integrity and assurance justifications in Appendix B.17.

2.10. Step 10: Comprehensive Safety Portfolio (CSP)

The final stage compiles all evidence generated across the previous SORA steps into a CSP. Although a formal one was not submitted to the KCAA, the materials produced for this project (operational description, risk assessment, and permit-application documents) effectively constituted the project’s version of a CSP. Together, they demonstrated how the operation addressed the safety claims and derived requirements for a SAIL II context. Future iterations would benefit from a structured compliance matrix to explicitly map each claim to its supporting evidence and improve traceability within the CSP.

3. Procedures Setup and Development

Building on the SORA-based risk framework, this section describes how safety requirements were translated into operational practice during the January 2025 field campaign at Ol Pejeta Conservancy, including organisational setup, coordination workflows, and standard operating procedures co-designed by safety specialists and field biologists.
Methodological scope of efficiency metrics: All efficiency metrics are derived from retrospective operational comparisons rather than controlled experiments. Baselines reflect conservative early-campaign configurations, while reduced configurations result from validated adaptations introduced with increased operational experience.

3.1. Crew Configurations and Roles Refinement

Operations initially employed a conservative crew structure with one pilot, one co-pilot, and dedicated airspace and ground observers per UAS (Figure 7a), ensuring redundancy and clear task separation during procedure validation and establishing a baseline for subsequent crew-scaling decisions. As operational confidence increased, observers were shared between teams operating from the same site (Figure 7b), with overlapping monitoring sectors allowing one observer pair to provide full coverage without exceeding workload limits.
This Multi-UAS setup was used when two teams co-located, typically during coordinated missions. It reduced staffing from 8 to 6 people, corresponding to an observed 25% reduction, without observed safety degradation, through defined sectors and coordinated timing. Table 6 summarises crew-size progression.
For swarm operations, 3 UAS flew synchronised missions using identical checklists, allowing the co-pilot role to be shared through centralised oversight (Figure 7c). This setup required 6 operators for 3 UAS, a 50% reduction relative to the initial configuration. By contrast, independent multi-UAS missions retained dedicated co-pilots because differing objectives required continuous availability for monitoring and emergency response.
During the extended campaign (February–June 2025), biologists operated in separate areas and required independent teams. Lower personnel availability and long-duration missions made larger crews impractical, so the co-pilot and airspace-observer roles were merged resulting in a three-person crew per UAS (Figure 7d). Across four teams, staffing decreased from 16 to 12 people (25% reduction). Because this combined role increased cognitive workload and reduced airspace-awareness robustness, maximum altitude was limited to 250 ft (75 m) AGL to reduce the likelihood of encounters with crewed traffic.
Overall, crew structures were simplified progressively as operational evidence accumulated, enabling reduced staffing while maintaining equivalent safety assurance.

3.2. Operations Planning and Coordination

Daily morning and afternoon briefings structured the overall coordination of up to 5 concurrent teams. These map-based sessions used the conservancy’s predefined patrol blocks to allocate scientific tasks, assign personnel and vehicles, and confirm platform availability. Patrol blocks were selected to avoid spatial overlap. When two teams required the same area, they merged and conducted the activity as a coordinated multi-UAS operation, with pilots positioned together to maintain direct verbal communication.

3.2.1. Third-Party Coordination

Team movements were reported to the Ol Pejeta radio room upon departure and return to maintain awareness of active UAS operations and to support rapid incident response. External communication with ATC was centralised through a single safety manager via mobile phone. ATC was contacted once before and once after each operational window, and the conservancy was treated as a single UAS operation for these exchanges, removing the need for team-level notifications.

3.2.2. Digital Coordination with WildOps

To support airspace coordination, a lightweight digital UTM prototype, WildOps (https://github.com/GuyMaalouf/WildOps-public, accessed on 29 January 2026), was trialled during the campaign. Pilots submitted planned missions by specifying the operation type (VLOS/BVLOS), time window, and take-off location, which were visualised as airspace volumes for approval by the safety manager.
In practice, this workflow was poorly aligned with field operations: although patrol blocks were assigned in advance, take-off locations were typically determined only after arriving on site and locating target animals, making pre-entry of coordinates impractical. On-site use required a laptop and mobile hotspot, increasing setup time, reducing usability in bright outdoor conditions, and adding workload during time-critical mission phases, while the lack of integrated positioning on laptops further complicated location entry.
Operationally, the safety manager required only confirmation that teams remained within the authorised flight geography and sufficiently separated from one another. This was more efficiently achieved by sharing a GPS pin via WhatsApp directly from the pilot’s mobile device, enabling rapid manual verification without detailed airspace visualisation or additional hardware.
Overall, the trial illustrates that desktop-based, pre-flight UTM workflows are poorly suited to dynamic conservation environments. Effective coordination in such contexts requires mobile-first tools with minimal user input, automatic position reporting, and interfaces designed for rapid, in-field decision-making rather than pre-planned submissions.

3.3. Operational Procedures, Iterations and Refinements

Field activities followed standard procedures spanning planning, pre-flight, in-flight, and post-flight phases, supported by contingency and emergency procedures. To manage these consistently across multiple operation types, the WildProcedures (https://github.com/GuyMaalouf/WildProcedures-checklist-generator, accessed on 29 January 2026) software was introduced. It maintained a central JSON (JavaScript Object Notation) database in which procedures were tagged by operation type (day/night, VLOS/BVLOS, with/without remote observer) and number of UAS (single, multiple, or swarm). A single command generated (i) a detailed procedures document and (ii) a compact field checklist. This automated approach replaced numerous static templates used during the June 2024 campaign and enabled rapid iteration, traceability, and customisation.

3.3.1. Adaptation Across Operation Types

Procedures were adapted to reflect differences in visibility, communication requirements, observer roles, and platform coordination, while maintaining a consistent core safety structure across all missions. Table 7 summarises how steps and equipment were tailored to match each operation type.

3.3.2. Measured Efficiency Gains from Customisation

Table 8 reports the observed reduction in checklist items achieved through customised procedures (excluding contingency and emergency protocols), showing an average decrease of about 18%. This reduction serves as a practical proxy for time savings.
Figure 8 shows that all efficiency gains occur before take-off, where streamlining has the greatest operational impact. These stages are time-sensitive, as rapid preparation affects the ability to observe or track wildlife.

3.3.3. Evolution of Procedures over Time

Procedures were refined iteratively through co-development between safety specialists and field biologists to streamline workflows while maintaining safety. Table 9 summarises the main areas of improvement and their outcomes.

4. Field Trials & Observations

The field trials presented in this section include both the WildDrone Hackathon operations conducted at Ol Pejeta Conservancy in January 2025 and the extended field campaigns that followed between February and June 2025. Together, these missions spanned diverse operational conditions and team configurations, providing a broad empirical basis for evaluating the practical application of the SORA-based safety framework introduced in Section 2. Rather than analysing individual missions in isolation, the trials are used to identify recurring operational constraints and mitigation patterns that inform the cross-cutting discussion in Section 5. They also support the operational insights discussed in Section 5, where five recurring constraints and their management strategies are examined:
(A) 
Large teams limit scalability but can be reduced safely through gradual optimisation;
(B) 
Repeated missions improve efficiency but require training to sustain vigilance;
(C) 
Range limits create time pressure but expansion depends on safe airspace integration;
(D) 
Environmental factors elevate operational risk and require crew-safety measures;
(E) 
Co-development ensures procedures remain practical and field-ready.
These observations illustrate how regulatory planning translated into field practice and provide the empirical grounding for the synthesis and generalisation presented in Section 5.

Summary of Field Trial Cards

Each operation was documented using a standardised Field Trial Card, ensuring consistent reporting of objectives, procedures, and observations. Table 10 summarises the missions at a high level, while Appendix C provides the full operational details. Together, they demonstrate how recurring patterns observed across heterogeneous missions underpin the higher-level discussion of safety, scalability, and operational trade-offs in Section 5.

5. Discussion

This section synthesises the main findings and addresses the research questions (Section 1.3), drawing on quantitative results and qualitative observations from Section 2, Section 3 and Section 4. It interprets how SORA 2.5 can guide BVLOS operations in protected areas characterised by low population density, limited infrastructure, and dynamic field conditions, and extracts transferable insights for other non-standard operational environments with comparable ground and air risk profiles, while recognising that quantitative efficiency gains are context-dependent.
  • RQ1. How Can SORA 2.5 Guide the Planning of BVLOS Operations in Conservation Areas?
The findings indicate that SORA 2.5 can guide BVLOS planning in conservation areas by clarifying dominant ground- and air-risk drivers and supporting proportionate mitigation strategies. As illustrated in Section 2, the framework helped distinguish risks requiring strategic spatial mitigations from those manageable through field procedures, informing decisions on flight exclusion areas, separation from aerodromes and roads, and conditions under which night operations remained acceptable. While specific mitigations remain context-dependent, this SORA-guided reasoning is applicable to other low-density, time-sensitive deployments where air risk is managed procedurally rather than through dense supporting infrastructure, such as remote environmental monitoring, disaster response, and search-and-rescue operations [33,34,35,36].
The assessment resulted in a sail II classification, after which operational safety was delivered primarily through structured field procedures. A retrospective review of relevant OSOs showed broad consistency with sail II expectations, indicating that well-designed field practices can achieve outcomes compatible with the framework. Future campaigns should formalise this alignment through more comprehensive OSO documentation.
A continuing limitation is the absence of reliable real-time air-traffic information, which reduces confidence in air-risk assumptions [37,38]. Progress in such environments will depend on improved airspace situational awareness, particularly through simple, affordable, and privacy-preserving Electronic Conspicuity (EC) solutions.
  • RQ1.1. How Can SORA 2.5 Ground-Risk Approaches Be Used in Conservation Settings, and How Do They Compare in That Context?
  • A—Population estimation relies more on local knowledge than modelling
Three population-density estimation approaches were compared against post-campaign daily administrative records used as ground truth, collected after more than 260 flights. The qualitative method provided reasonable first estimates but remained subjective where prior field knowledge was limited, while the bottom-up approach yielded similar values but required access to camp records that may not always be available. Raster-based estimates aligned only incidentally with these methods, as nearby village populations spilled into the conservancy and transient groups such as tourists and rangers, who constituted most people present during operations, were undercounted. Ground-truth observations confirmed this mismatch, revealing concentrated activity near Sweetwaters Camp that none of the models captured. Overall, reliable population inputs for SORA applications in conservancies require direct engagement with site managers and, where possible, on-site reconnaissance; raster products should therefore be treated as a secondary reference when field data cannot be obtained [39].
  • B—Raster-based population estimates have limitations
The raster analysis highlighted three factors influencing intrinsic ground-risk classification. First, grid resolution affected apparent density: at Ol Pejeta, WorldPop estimates ranged from 105 ppl/km2 at 100 m to 53 ppl/km2 at 500 m, with 200 m providing the most representative scale in line with SORA Annex F guidance [40]. Second, maximum-cell values overstated exposure, as isolated 100 m cells exceeded 100 ppl/km2 while 99% of the area remained below 37 ppl/km2, suggesting percentile-based thresholds may provide a more stable representation. Third, global rasters omitted transient activity, which dominated human presence in the conservancy. Together, these factors indicate that raster-based estimates require careful interpretation and supplementation with local knowledge.
  • C—Annex F analytical estimation provides a more representative assessment
Using a representative density, the intrinsic ground-risk class was computed with both the tabulated and analytical SORA Annex F methods. The lookup table placed the 3.8 m UAS just above a category threshold, resulting in iGRC 5, whereas the continuous analytical method yielded iGRC 4. This one-class difference reflects the conservative nature of tabulated approaches near boundaries; while it did not affect the resulting SAIL in this case, it could ease downstream requirements in other contexts. Analytical estimation is therefore preferable near boundary conditions, as it provides a more proportional assessment while remaining feasible with standard computational tools.
  • RQ1.2. Which Safety Constraints Affect Conservation Fieldwork, and How Can They Be Addressed?
This section outlines the main safety constraints observed during field operations and how they can be addressed within a SORA-guided framework.
  • A—Large teams limit scalability but can be reduced safely through gradual optimisation
Early missions relied on large teams, increasing coordination overhead and limiting scalability. Roles were progressively combined (e.g., shared observers and merged co-pilot/airspace-observer), enabling reductions without overloading individuals [41]. Crew optimisation should proceed incrementally, with clear role definitions and checks that reductions do not degrade airspace awareness, supported by mitigations where needed.
  • B—Repeated missions improve efficiency but require training to sustain vigilance
Daily repetition improved coordination and reduced setup times as teams became familiar with checklists and terrain. However, routine operations and increasing automation risked reduced vigilance, particularly in multi-UAS contexts [42]. In-flight checklists therefore prompted active cross-checks of telemetry, airspace status, and observer reports. Sustaining efficiency without loss of alertness requires structured and recurrent training.
  • C—Range limits create time pressure but expansion depends on safe airspace integration
Limited range created time pressure when animals moved quickly, highlighting the need for efficient coordination and repositioning. These constraints were driven primarily by airspace integration: many crewed aircraft over conservancies are non-cooperative and electronically invisible, requiring human observers to maintain separation. Extended-range missions (≤2 km by day, ≤5 km at night) therefore relied on remote airspace observers to maintain visual coverage, improving safety but increasing logistical complexity. Future BVLOS expansion depends on improved airspace-situational-awareness systems capable of detecting cooperative and non-cooperative aircraft; until then, hybrid approaches combining digital tools and observers remain the most practical solution.
  • D—Environmental factors elevate operational risk and require crew-safety measures
Vegetation, wind, wildlife proximity, and night operations affected visibility, positioning, and line-of-sight continuity [43], requiring adjustments to launch sites and observer placement. Environmental limits were encoded in checklists, while crew-safety risks were managed through field protocols. Procedures should explicitly define the environmental conditions under which they remain valid, integrating operational and crew-safety considerations.
  • E—Co-development ensures procedures remain practical and field-ready
Procedures developed during early missions were conservative and poorly adapted to field realities. During the January 2025 campaign, collaborative refinement by safety specialists and field teams removed redundancies, reordered steps, and strengthened contingency responses, including additional checks following an incoming crewed aircraft event. Iterative co-development maintains alignment with SORA expectations while ensuring procedures remain usable in daily conservation operations.
  • RQ2. How Should Safety Procedures Be Designed to Meet the Needs of Conservation Fieldwork?
Developing safety procedures for conservation operations requires balancing regulatory requirements with field practicality. This section presents a compact methodology for designing field-ready procedures that remain clear, usable, and safe in dynamic field conditions, and that is applicable to other low-density, time-sensitive deployments.
1. 
Define scope and inputs: Specify operational scope (normal, contingency, emergency) and context (terrain, airspace, wildlife rules, UAS type, crew roles), consistent with SORA Annex E OSO #08(a) [9], ISO 21384-3 [44], and ICAO Doc 10019 [45].
2. 
Design the checklist family: Create checklists for planning, pre-/post-operation, all flight phases, emergency, and contingency. Keep emergency and contingency lists readily accessible, and maintain both detailed procedures and concise field checklists [44,45].
3. 
Apply clear placement rules and initiation anchors: Shift tasks that can be completed off-site to pre-operation; avoid repeated power cycles within a phase; use full checks only for the first flight and a reduced set for subsequent flights. Define initiation anchors for each checklist (e.g., pre-operation at the vehicle, first flight on arrival, subsequent flights before take-off, post-flight at landing) [46].
4. 
Set the right level of detail: Keep lists short and readable. Combine low-workload actions that occur together, separate safety-critical steps, use clear action verbs, avoid negations, and do not cluster demanding actions at the same moment [46,47].
5. 
Express environmental limits as field cues: Translate wind, visibility, terrain, and vegetation constraints into simple observable cues [9,45] so crews can apply limits without relying on instruments alone.
6. 
Minimise the “subsequent flight” checklist: After configuration and calibration are confirmed [9,46], retain only essential recurring steps: logging, power-up, battery and SD-card changes, error checks, GNSS and link confirmation, brief weather scan, team brief, go/no-go decision, take-off call, and immediate post-lift performance check.
7. 
Manage crew fatigue and workload: Apply fatigue-management principles (rest, hydration, role rotation, recovery days) rather than fixed-hour limits. Include the IMSAFE check in pre-operation and launch phases to confirm fitness to operate [9,45].
8. 
Separate emergency, contingency, and Emergency Response Plan (ERP): Define emergency procedures for immediate abnormal events, contingency procedures for predictable degradations, and the ERP for post-accident actions (e.g., crash, fire, injury, airspace incident), including relevant contact details [9,44,45].
9. 
Ensure formatting and legibility: Apply human-factors design principles: clear typography, left alignment, sufficient spacing, consistent structure, strong contrast, and visual emphasis on high-importance actions without implying optionality [46,47,48].
10. 
Validate and refine iteratively: Test procedures via table-top reviews and limited flights, refine them through daily debriefs, and maintain version control and change logs. Where higher assurance is required, follow SORA Annex §E.3 [9] and accepted means of compliance such as ASTM F3178-16 [49].
  • RQ2.1. How Much Efficiency Can Be Gained by Tailoring Procedures to Specific Missions?
Tailoring procedures to mission type reduced the number of checks per operation by an average of about 18%, with most savings occurring before take-off, particularly during pre-flight and first-flight phases. Although this reduction is only a proxy for time saved and was not derived from a formal time–motion study, it indicates that modest adjustments to preparation steps can yield meaningful efficiency gains in daily fieldwork [47].
These gains resulted from aligning procedures with operational context. Differences in range, time of day, and number of UAS produced distinct risk profiles that warranted targeted adaptations: night missions required different equipment and omitted day-specific checks, while multi-UAS operations introduced coordination and vertical-separation checks to prevent conflicts during take-off and landing. Such tailoring removed irrelevant steps without compromising safety, and similar differentiation could extend to UAS-specific procedures as platform data become more standardised.
Using a centralised database in WildProcedures (https://github.com/GuyMaalouf/WildProcedures-checklist-generator, accessed on 29 January 2026) ensured that customisation did not erode standardisation. Automatically generating tailored checklists reduced checklist habituation [46,47] by removing items with no operational relevance, improving both efficiency and operator vigilance.
Overall, procedural tailoring offers the greatest benefit in operations with variable configuration or risk, such as changing range, complexity, or number of UAS, which is typical of field-deployed, time-sensitive missions. For repetitive single-UAS operations under uniform conditions, efficiency gains are more limited.
  • RQ2.2. Which Procedural Elements Can Be Automated, and How Does Automation Affect Crew Workload and Reliability?
Automation can reduce workload by handling routine tasks, improving situational awareness, and reducing manual errors. Its greatest value lies in planning and pre-flight phases, where information gathering and verification dominate. In-flight tools can support vigilance through periodic prompts, while packing, inspection, and post-flight tasks remain largely physical and offer limited scope for automation. Similar task boundaries have been reported in other time-sensitive field operations, including emergency response and remote environmental monitoring, where preparation benefits most from automation while in-field decision-making remains human-centred.
Fully automatable elements include retrieving airspace and weather data, checking crew qualifications, and generating mission-specific checklists. Partial automation is appropriate near operational limits, where systems can flag uncertainty but require human confirmation. Safety briefings, final go/no-go decisions, and emergency coordination with ATC must remain human-led.
Automation also introduces human-factors risks, including reduced attention (automation complacency), over-trust (automation bias), and skill degradation (out-of-the-loop effects) [50,51,52,53]. Mitigation requires guardrails such as confirmation prompts, challenge–response calls, and periodic checks that maintain operator engagement.
Overall, automation can reduce workload and omissions while supporting situational awareness, but it should complement rather than replace human judgement, particularly during contingencies. Future work should examine how specific automation features affect workload, vigilance, and reliability in real operations.
  • RQ3. How Can BVLOS Operations Be Scaled to Multiple Teams While Preserving Safety in the Field?
Scaling multi-team BVLOS operations requires clear spatial organisation, predictable workflows, and shared situational awareness [54]. The practices below summarise methods applied during five-team field operations (over 260 flights and 60 h) and are relevant to other low-density, time-sensitive deployments where multiple crews operate concurrently under procedural airspace separation. These insights are based on repeated operational use and qualitative safety outcomes rather than controlled comparative experiments.
1. Defined flight zones support effective deconfliction: A shared operational map defining authorised flight areas and contingency zones provides a common spatial reference and reduces overlap [55]. Dividing the area into clear zones simplifies coordination without relying on precise GPS positioning.
2. Operational windows reduce coordination load: Fixed activity windows (e.g., morning, afternoon, night) streamline logistics, improve resource sharing, and reduce the likelihood of overlapping operations [55].
3. Centralised supervision strengthens operational safety: A central safety manager maintains oversight across teams [54], confirms compliance with authorised geographies, and acts as the single point of contact with ATC and external authorities, preventing inconsistent reporting.
4. Robust coordination is essential for safe separation in shared airspace: When multiple UAS share airspace, co-located pilots can coordinate take-off and landing verbally, supported by standard vertical-separation rules. In multi-UAS missions this maintains independent trajectories, while swarm operations rely on synchronised checklists and a shared mission objective.
5. Reliable communication ensures safe coordination: Communication channels should be verified before each flight, with multiple technologies used to provide redundancy and maintain connectivity between teams.
6. Continuous feedback sustains safety at scale: Debriefs after each operational window identify coordination issues and inefficiencies. Feeding this information back into procedures and checklists helps prevent gradual erosion of safety margins as operational tempo increases.
  • RQ3.1. How Can Crew Configurations Be Optimised to Improve Scalability While Maintaining Safety, and What Trade-Offs Arise?
Optimising crew configurations requires reducing team size without undermining workload balance or situational awareness. Field experience showed that once procedures stabilise and task demands become predictable, roles can be merged progressively in a structured manner [56]. Similar crew-scaling dynamics have been reported in other field-based BVLOS contexts relying on procedural airspace separation rather than infrastructure-supported detect-and-avoid, indicating applicability beyond conservation settings. The principles below summarise how teams can scale while managing safety trade-offs.
1. 
Begin with conservative crew configurations and iterate toward efficiency: Early missions should use larger teams to keep workload low while procedures mature. As processes stabilise, compatible roles can be merged through iterative review without loss of situational awareness [57].
2. 
Balance operational needs with safety trade-offs: Smaller teams may be necessary under field constraints but increase workload and reduce redundancy. When reductions are unavoidable, compensatory measures such as limiting altitude, range, or mission complexity should be applied, and reductions implemented only once their effects are understood.
3. 
Leverage shared roles in multi-UAS and swarm operations: In multi-UAS missions, observers can be shared if coverage areas are clearly defined. Swarm operations allow further role sharing (e.g., co-pilots) when UAS follow the same checklist and timing, provided responsibilities remain explicit.
4. 
Merge roles that share a single operational focus: Role consolidation is most effective when tasks contribute to a single operational focus. For example, co-pilot and airspace-observer roles may be combined due to their shared aviation-safety objective, whereas wildlife-observer roles require independence. Clear responsibility boundaries reduce cognitive switching and simplify qualification.
5. 
Maintain vigilance through cross-checks: Routine operations can reduce alertness; short challenge–response calls help maintain focus and prevent complacency during low-workload phases.
  • RQ4. What Needs to Happen for Field-Supported BVLOS Operations to Become Fully Remote?
This discussion reflects the authors’ perspective on potential pathways toward remote BVLOS operations and is intended as an interpretative outlook rather than a statement of regulatory fact.
Transitioning from field-supported to fully remote BVLOS operations requires progressively replacing on-site roles with reliable airspace integration, communication, and autonomy. Drawing on evidence from this study, prior work on remote UAS integration [58,59], and current regulatory trends, this section outlines a plausible and transferable pathway rather than quantitative performance claims. The progression is incremental: extending range with minimal personnel, reducing local roles as assurance grows, and ultimately enabling remote or autonomous concepts such as UAS-in-a-box. Although derived from conservation deployments, these constraints and pathways apply to other low-density, time-sensitive operations, including rural disaster response, search and rescue, and remote environmental monitoring.
A. 
Airspace integration as the primary enabler
The main barrier to remote BVLOS operations is airspace integration, particularly in regions with mixed cooperative and non-cooperative traffic and limited surveillance infrastructure. Under the SORA TMPR framework [9], operators must detect a significant proportion (50∼90%) of intruding crewed aircraft, yet poor characterisation of traffic behaviour in regions such as sub-Saharan Africa prevents meaningful verification of detection performance. As a result, operational range remains constrained by visual observer coverage.
Emerging regulatory approaches emphasise EC for cooperative airspace management. The U.S. Part 108 draft rule links right-of-way to broadcast status [60], Europe’s U-space framework similarly relies on EC [61], and ADS-L provides a lightweight transmission option [62,63]. Trials such as the UK i-Conspicuity programme demonstrate detection ranges beyond 10 km, though cost, privacy, and interoperability remain barriers [64,65,66]. Universal EC adoption offers the most scalable path, while non-cooperative sensing suits specialised contexts [67].
B. 
Evolution of air-risk methodology
While SORA 2.5 strengthened ground-risk and containment structures, air-risk logic (ARC and TMPR) remains conservative. Field experience shows reliance on procedural mitigations and human-centred responses. As EC adoption increases, detect-and-avoid systems will require staged validation, beginning with conservative separation and relaxing criteria as evidence accumulates, mirroring earlier scaling of field-supported multi-UAS operations.
C. 
Connectivity and command resilience
Beyond airspace integration, Command and Control (C2) resilience becomes the next constraint. Current operations rely on RF line-of-sight links over 2–5 km, whereas remote missions require redundant architectures combining RF, cellular, or satellite links. Increasing range will favour higher-level intent-based control over continuous low-level inputs. Studies such as GENIUS indicate that 5G can meet safety-critical requirements, though rural coverage remains uneven [68]. Autonomous functions must tolerate short link losses and execute predefined contingencies, consistent with OSO #06 and OSO #13.
D. 
Incremental pathway toward remote operations
Progress toward remote BVLOS operations should follow a staged approach: start conservatively, validate performance, and expand complexity gradually. Interoperable EC and shared airspace situational awareness form the immediate foundation, enabling advances in connectivity and autonomy through evidence-based testing. Remote operations thus represent a continuation of learning cycles toward safer, more scalable UAS integration.

6. Conclusions

This study examined how SORA 2.5 can guide multi-team BVLOS operations in protected, low-density conservation areas, using field campaigns conducted in Kenya as an empirical basis. Rather than proposing a new risk framework, the work illustrates how SORA outputs can be interpreted and operationalised in environments characterised by limited infrastructure, transient populations, and procedural airspace management.
The analysis combined ground- and air-risk assessment with operational evidence from over 260 flights and more than 60 h of activity. Qualitative, bottom-up, and raster-based population estimates all indicated lightly populated conditions, but ground-truth records showed that global rasters can under-represent transient exposure associated with tourism and ranger activity. This reinforces the need for local data when assessing ground risk in conservation settings. Near threshold cases, the Annex F analytical method produced a less conservative intrinsic Ground Risk Class than the tabulated approach, while a retrospective review against Annex E clarified which Operational Safety Objectives were satisfied in practice and where further evidence is required. Although derived from a single conservancy, these risk-assessment challenges and trade-offs are representative of other low-density, time-sensitive field deployments.
Operationally, the campaigns demonstrated that structured spatial planning, shared procedures, and central oversight can support concurrent BVLOS missions with multiple teams. Progressive crew restructuring reduced team size by approximately 25–50% while maintaining observed safety margins, and mission-specific procedures generated using WildProcedures reduced checklist length by an average of 18%, with most gains occurring before take-off. These figures are indicative rather than statistically validated, but they show how procedural tailoring can improve efficiency without eroding safety. A lightweight coordination tool (WildOps) supported situational awareness but proved ill-suited to highly mobile crews and intermittent connectivity, highlighting that digital tools must be designed around field constraints rather than control-room assumptions. The resulting ten-step procedure-design framework provides a reusable, field-ready structure for translating SORA objectives and human-factors guidance into practical checklists for conservation and similar low-infrastructure operations.
Taken together, the findings show how SORA-informed risk assessment, locally grounded population estimation, compact crews, and tailored procedures can support scalable BVLOS operations while preserving safety transparency. For regulators and practitioners, the study illustrates how SORA 2.5 can be adapted to fenced reserves and procedurally managed airspace, how analytical ground-risk methods can avoid unnecessary conservatism, and how lightweight procedure-generation tools can support assurance arguments in the field.

Limitations and Future Work

This work is limited to a single conservancy, a specific regulatory context involving military-controlled airspace, and a restricted set of UAS platforms. Efficiency and safety claims are based on checklist structure, crew configuration, and observed operations rather than formal time–motion studies or incident statistics. Future work should strengthen evidence for partially satisfied Operational Safety Objectives, particularly those related to tactical mitigation performance, through systematic measurement of workload, timing, and safety events. The procedure-design approach and WildProcedures should be extended to additional platforms and environments, while coordination tools such as WildOps require mobile-first, connectivity-aware redesign to support wider EC adoption, improved detect-and-avoid performance, and resilient communications beyond short-range radio links, enabling a gradual transition to fully remote BVLOS operations.   

Author Contributions

Conceptualization, G.M., K.J. and U.P.S.L.; methodology, G.M., T.S.R., D.R.G., M.W., B.R.C., U.P.S.L. and K.J.; software, G.M.; validation, T.S.R., D.R.G., M.W., B.R.C., U.P.S.L. and K.J.; formal analysis, G.M. and K.J.; investigation, E.P., B.R.C., S.A., E.G.A.R., K.M., T.v.d.S., L.L.-D., C.R.S.-J., C.A.M.C., V.S., E.I., J.K., D.N.N. and W.N.; resources, T.S.R., D.R.G., M.W., B.R.C., U.P.S.L. and K.J.; data curation, G.M., E.P., S.A., E.G.A.R., K.M., T.v.d.S., L.L.-D., C.R.S.-J., C.A.M.C., V.S., E.I., J.K. and D.N.N.; writing—original draft preparation, G.M.; writing—review and editing, G.M., T.S.R., D.R.G., M.W., U.P.S.L., B.R.C., E.P., S.A., E.G.A.R., K.M., J.H.J., T.v.d.S., L.L.-D., C.R.S.-J., C.A.M.C., V.S., E.I., J.K., D.N.N. and K.J.; visualization, G.M.; supervision, K.J., U.P.S.L., T.S.R., D.R.G., M.W. and B.R.C.; project administration, T.S.R., D.R.G., M.W., U.P.S.L., B.R.C., E.P. and K.J.; funding acquisition, T.S.R., D.R.G., M.W., U.P.S.L., B.R.C., E.P. and K.J. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by the WildDrone MSCA Doctoral Network (EU Horizon Europe, Grant No. 101071224); the EPSRC project “Autonomous Drones for Nature Conservation Missions” (EP/X029077/1); the AI Institute ICICLE (NSF Award #2112606); and the Imageomics Institute (NSF HDR, Award #2118240). B.R.C. also acknowledges support from the University of Konstanz Investment Grant programme and the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) under Germany’s Excellence Strategy—“Centre for the Advanced Study of Collective Behaviour” EXC 2117–422037984.

Data Availability Statement

Publicly available inputs, including regulatory documents, population raster datasets, and manufacturer specifications, are cited and linked within the manuscript. Operational materials generated during the WildDrone field campaigns, such as procedures, risk assessment artefacts, and Field Trial Cards, contain sensitive regulatory and location-specific information and are therefore not fully publicly available. Redacted and representative examples are provided as Appendix A, Appendix B and Appendix C.

Acknowledgments

The authors sincerely thank the Kenya Wildlife Services, the Ol Pejeta Conservancy management and staff, Kenya Flying Labs (especially Cleopa Otieno), the Kenya Civil Aviation Authority (particularly Francis Kigen), the local Kenya Air Force Air Traffic Control, and the Wildlife Research and Training Institute for their invaluable support during this project.

Conflicts of Interest

The authors declare no conflicts of interest. Author Saadia Afridi was employed by the company Avy B.V. The remaining authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.

Appendix A. Kenyan UAS Regulations and Permit Process

Introductory Note: This supplementary appendix provides the technical material supporting the main article, covering regulatory, methodological, and operational aspects omitted for brevity. Appendix A outlines the Kenyan UAS regulatory framework and the permit process for temporary import and BVLOS authorisation. Appendix B presents the full SORA 2.5 application, including volume definitions, population-density estimation methods, intrinsic and mitigated ground-risk assessments, TMPR analysis, SAIL determination, adjacent-area evaluation, and containment requirements. Appendix C compiles the Field Trial Cards, summarising mission procedures and operational lessons from the WildDrone activities. Together, these appendices form the technical basis for the regulatory analysis and operational insights discussed in the paper.

Appendix A.1. Civil Aviation UAS Regulatory Framework

The regulation of UASs in Kenya is defined by the Civil Aviation Unmanned Aircraft Systems Regulations 2020 (Legal Notice No. 42, Kenya Gazette Supplement No. 34, 30 March 2020). These regulations classify operations into three categories according to the risk posed to persons, property, and airspace:
  • Category A (Low Risk): Restricted to Visual Line Of Sight (VLOS) operations at or below 400 ft AGL with a Max Take-Off Weight (MTOW) ≤ 25 kg. A lateral separation of at least 50 m must be maintained from uninvolved persons, buildings, and objects. Operations must occur in segregated airspace unless expressly authorised by the KCAA.
  • Category B (Medium Risk): Also limited to VLOS (including extended VLOS), but permits operations exceeding certain Category A constraints. These may occur in non-segregated airspace, provided they remain clear of controlled or restricted zones unless authorised.
  • Category C (High Risk): Covers high-complexity operations, including BVLOS flights and missions in controlled airspace, requiring integration with ATC, compliance with the Civil Aviation (Rules of the Air) Regulations, and a valid Certificate of Airworthiness.
All categories require prior KCAA approval, including a temporary import permit and an operational authorisation. Commercial activities additionally require a valid Remote Operator Certificate (ROC).
At the time of our operations, routine authorisation of BVLOS missions was not available due to the absence of a national UTM system. However, because flights occurred within military-controlled airspace, the KCAA granted an exemption contingent on approval by the KAF ATC. Consequently, BVLOS operations required coordination with both civil and military regulators.
Details of the authorisation workflow and submitted documentation are summarised in the main paper. All templates and forms are available in our open-access repository (https://github.com/GuyMaalouf/wilddrone-hackathon-2025-bvlos-ops, accessed on 29 January 2026).

Appendix A.2. Permit Application Requirements

This section summarises the documentation submitted to the KCAA and KAF to obtain temporary import and operational permits for the January 2025 campaign.
Table A1. Documentation Required to Apply for a UAS Temporary Import Permit.
Table A1. Documentation Required to Apply for a UAS Temporary Import Permit.
Document TypeDetails
UAS DetailsMake, model, serial number, MTOW
Arrival and DepartureOperating airline, flight number, dates and times of entry and exit
Pilot PassportPassport copy of the drone operator
Pilot CertificateRemote pilot competency certificate
UAS InsuranceProof of third-party liability insurance
UAS PhotographsPhotos of each UAS and visible serial numbers
Table A2. Documentation Required to Apply for a UAS Operational Permit.
Table A2. Documentation Required to Apply for a UAS Operational Permit.
RequirementDetails
Proposed OperationOperation map, flight geography, platform specifications, ground/air risk identification and mitigations, team structure, and SORA-based risk assessment
Temporary Import PermitProof of import approval for all platforms
ROC LeaseLease agreement under the ROC of KFL
Letter from ConservancyFormal letter of support from Ol Pejeta Conservancy
KWS ApprovalLetter of no objection from the Laikipia regional office of the KWS
Wildlife Research PermitPermit issued by the WRTI
Research LicenceNational Science and Technology Research License from NACOSTI

Appendix B. Detailed Application of the Ten-Step SORA Methodology

Appendix B.1. SORA Semantic Map and Volume Definitions

Before applying SORA Step 2, it is necessary to define the spatial model used for risk containment and footprint calculations. The SORA semantic map in Figure A1 outlines five operational volumes defined by the Joint Authorities for Rulemaking on Unmanned Systems (JARUS) methodology: flight geography, contingency volume, ground risk buffer, containment area, and adjacent area.
Figure A1. SORA semantic map for the January 2025 field campaign. The figure shows the spatial volumes used for containment and ground/air-risk assessment: (1) Flight geography (green); (2) Contingency volume (orange), defined by a 1.5 km buffer based on the fastest UAS performance; (3) Ground-risk buffer (red), a 400 ft (120 m) band aligned with the maximum flight altitude; (4) Containment area (purple), the 1 km band used in Step 8 to verify containment and detect assemblies; (5) Adjacent area (light blue), used to evaluate exposure beyond the containment area; (6) Air-risk buffer zones (ruby red), lateral and vertical separations from nearby aviation activity; (7) Campgrounds (yellow), treated as sensitive zones and excluded during ground-risk mitigation.
Figure A1. SORA semantic map for the January 2025 field campaign. The figure shows the spatial volumes used for containment and ground/air-risk assessment: (1) Flight geography (green); (2) Contingency volume (orange), defined by a 1.5 km buffer based on the fastest UAS performance; (3) Ground-risk buffer (red), a 400 ft (120 m) band aligned with the maximum flight altitude; (4) Containment area (purple), the 1 km band used in Step 8 to verify containment and detect assemblies; (5) Adjacent area (light blue), used to evaluate exposure beyond the containment area; (6) Air-risk buffer zones (ruby red), lateral and vertical separations from nearby aviation activity; (7) Campgrounds (yellow), treated as sensitive zones and excluded during ground-risk mitigation.
Drones 10 00178 g0a1
These volumes define the spatial boundaries used throughout the assessment. Their definitions, based on the official JARUS documentation [9], are:
  • Flight geography: The volume in which the UAS is intended to operate under normal conditions, defined horizontally and vertically by planned mission paths and operational constraints.
  • Contingency volume: A buffer surrounding the flight geography that accounts for off-nominal behaviour (e.g., navigation or link loss) in which the UAS remains controllable but deviates from the planned trajectory.
  • Ground-risk buffer: A horizontal buffer extending from the contingency volume, defined using a 1:1 rule relative to maximum altitude. It represents the area potentially affected by a ballistic descent and forms part of the intrinsic Ground Risk Class (iGRC) footprint.
  • Adjacent area: The region beyond the ground-risk buffer used to assess exposure to uninvolved people and determine the containment requirement.
  • Containment area: The first 1 km band of the adjacent area, used in Step 8 of the SORA to identify outdoor assemblies and verify containment performance.

Appendix B.2. Additional Notes on Buffer Selection and Design Choices

Unlike other SORA parameters, the contingency volume size is not prescribed by the JARUS guidance. It is the responsibility of the operator to define an appropriate buffer based on aircraft performance and operational context. Choosing a smaller contingency volume allows for a larger flight geography but leaves limited reaction time for the pilot or failsafe systems. This increases the risk of exiting the contingency volume, resulting in a loss of control scenario under SORA, which may trigger immediate termination procedures. In contrast, an overly large contingency volume, especially when applying a top-down approach, significantly shrinks the flight geography, possibly restricting mission feasibility.
By subtracting the contingency volume and ground risk buffer from the conservancy’s boundary, we delineated the flight geography. This yielded a conservative and bounded intrinsic Ground Risk Class footprint, while ensuring that areas with higher population density, such as nearby villages, were excluded from the operational volume. Campgrounds, shown in yellow on the semantic map, were also flagged as high-risk zones and are explicitly excluded from flights as part of the mitigation measures applied in SORA Step 3 (Ground Risk Mitigations).
This approach ensured that the UAS operational volume remained confined to safer areas. In contrast, a bottom-up approach—in which a mission-specific flight geography is initially defined, then expanded by adding contingency and ground risk buffers—can offer finer control over the desired operational area. However, it increases the likelihood of overlapping with populated or sensitive zones, potentially elevating the Ground Risk Class and triggering more stringent SORA Operational Safety Objectives (OSOs).

Appendix B.3. Qualitative Descriptors for Population Density

Table A3 provides the official qualitative descriptors used to support ground population density classification in Step 2 of the SORA methodology. These descriptors were adapted from Table 8 of Annex F [9] in the SORA 2.5 documentation and offer guidance on identifying population classes based on local characteristics.
Table A3. Qualitative Descriptors for Population Density (adapted from SORA 2.5, Annex F, Table 8 [9]).
Table A3. Qualitative Descriptors for Population Density (adapted from SORA 2.5, Annex F, Table 8 [9]).
D pop (ppl/km2)Qualitative DescriptorArea Description
Controlled Ground AreaControlled Ground/Extremely RemoteControlled access areas, or remote regions such as mountains, deserts, or large water bodies away from expected traffic.
<5RemoteForests, deserts, or sparsely settled land with approx. one small building per km2.
<50Lightly populatedSmall farms or residential areas with large lots (approx. 4 acres or 16,000 m2).
<500Suburban/Residential lightly populatedHomes and small businesses with large lots (approx. 1 acre or 4000 m2).
<5000Low density metropolitanApartments, commercial buildings, or small lots; buildings generally under 4 stories.
<50,000High density metropolitanDense urban centers with multistorey buildings and high population density.
≥50,000Assemblies of peopleMajor cities, large gatherings such as concerts or sporting events.
In the main text, we classified the Ol Pejeta Conservancy as “lightly populated” based on these descriptors. That classification was further validated using the quantitative methods described in Section 2.2.

Appendix B.4. Tourism-Based Estimation of Population Density

To support the population-density assessment required in SORA Step 2, we estimated the number of tourists likely present in Ol Pejeta Conservancy in January 2025. The estimate combines historical visitor data, post-COVID recovery trends, and seasonal patterns to derive a context-specific approximation from publicly available sources.
1.
Local Growth and COVID Impact.
We analysed annual visitor statistics for Ol Pejeta from 2016–2022 [19]. The sharp downturn in 2020–2021 reflects the COVID-19 impact, with partial recovery in 2022. To characterise baseline growth independently of the pandemic, we computed the pre-COVID Average Annual Growth Rate (AAGR) using 2016–2019 data:
A A G R = 1 3 y = 2017 2019 V y V y 1 V y 1 = 7 %
where V y is the observed number of tourists in year y.
2.
Adjustment Using Global Post-COVID Recovery Benchmarks.
To account for ongoing global recovery, we applied UN Tourism recovery factors for 2023–2025 [17,18]:
  • 2023: 84–92% of 2019 levels
  • 2024: 97–99% of 2019 levels
  • 2025: projected at 104–106%, obtained by applying the 7% AAGR to 2024 values
Projected values were computed using:
V ˜ y = V 2019 × f y
where V ˜ y is the projected tourist count for year y, V 2019 is the observed 2019 value, and f y is the relevant recovery factor.
3.
Projected Annual Totals.
Table A4 summarises observed and projected tourist numbers for 2016–2025, with lower and upper bounds for 2023–2025 based on UN Tourism scenarios. Figure A2 presents the same data with a confidence band and visual shading over COVID-affected years.
Figure A2. Projected annual tourist visits to Ol Pejeta Conservancy (2016–2025). Blue markers indicate observed values based on official Ol Pejeta annual reports. The grey band from 2019–2021 highlights the tourism downturn caused by the COVID-19 pandemic. From 2023 onward, projections are based on regional recovery rates published by the UN Tourism (expressed as a percentage of 2019 levels), combined with a local pre-COVID growth rate of 7%. A midline shows the central estimate, with a confidence band representing lower and upper recovery bounds. A dotted vertical line marks the transition from observed to estimated values.
Figure A2. Projected annual tourist visits to Ol Pejeta Conservancy (2016–2025). Blue markers indicate observed values based on official Ol Pejeta annual reports. The grey band from 2019–2021 highlights the tourism downturn caused by the COVID-19 pandemic. From 2023 onward, projections are based on regional recovery rates published by the UN Tourism (expressed as a percentage of 2019 levels), combined with a local pre-COVID growth rate of 7%. A midline shows the central estimate, with a confidence band representing lower and upper recovery bounds. A dotted vertical line marks the transition from observed to estimated values.
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Table A4. Annual tourist visit data and post-COVID projections for Ol Pejeta Conservancy.
Table A4. Annual tourist visit data and post-COVID projections for Ol Pejeta Conservancy.
Metric2016201720182019202020212022202320242025
Observed85,87488,842102,160111,24231,35965,91685,965
Lower Bound93,442107,905115,692
Upper Bound102,343110,129117,917
Midline97,893109,017116,805
4.
Seasonal Adjustment for January.
Because our operations took place in January, we applied a month-specific adjustment. January in central Kenya marks the start of the short dry season. Safari guidance for Ol Pejeta and Kenya describes December–March as a dry, favourable period with lower crowding and prices than the July–October peak [69,70,71].
We therefore used a seasonality factor s J a n = 1.0 with a conservative ± 10 % margin and computed average daily visitors as:
V Jan , y = V ˜ y 365 × s J a n = 320 ± 10 %
where V Jan , y is the estimated January daily presence. Applying the conservative +10% upper bound yields 352 tourists per day for January 2025.
5.
Estimating Localised Tourist Density at Camps.
For SORA Step 2, we then estimated the maximum localised density by assuming all tourists are concentrated at camps at night, when visitor clustering is highest.
a.
Number of camps:
Based on Ol Pejeta’s official accommodation listings, we identified ten active tourism facilities: Sweetwaters Serena Camp, Porini Rhino Camp, Ol Pejeta Bush Camp, Ol Pejeta Safari Cottages, Kicheche Laikipia Camp, Mutara Camp, Pelican House, Sanctuary Tambarare, River Camp, and The Stables [72].
b.
Tourist distribution:
Even distribution of 352 tourists across ten camps gives:
352 10 = 36 tourists per camp
c.
Camp staff:
Drawing on operational experience at The Stables, we conservatively assume 10 staff per camp, giving:
36 tourists + 10 staff = 46 people per camp
d.
Area of influence:
We bound each camp to a 1 km2 inhabited area, yielding a population density of:
46 1 km 2 = 46 people / km 2
This value remains below the SORA threshold of 50 people/km2 for a lightly populated area and supports our intrinsic ground-risk classification.

Appendix B.5. Raster-Based Estimation of Population Density

To complement qualitative and local estimates of ground population density, we evaluated publicly available gridded data from the WorldPop project. This appendix summarises the dataset, processing steps, and interpretation.
a.
Source Dataset:
We used the 2020 WorldPop raster for Kenya [20], which provides resident-population estimates at a ∼100 m (3 arc-second) resolution. Values are produced using a random forest-based dasymetric disaggregation method [39] that redistributes census counts using high-resolution covariates (night-time lights, building footprints, roads, land cover). The resulting raster gives the estimated number of residents per cell.
b.
Raster Processing:
A lightweight Python script extracted and analysed a local subset of the raster using:
Processing steps:
  • Clip raster to the conservancy boundary.
  • Convert native units (people per 0.01 km2) to people/km2.
  • Compute summary statistics at 100 m resolution.
  • Aggregate to 200 m and 500 m to assess grid-size effects, following Annex F of the SORA.
  • Visualise raster layers for inspection.
At 100 m resolution, the average density was 12.19 people/km2 and the maximum 104.84. Aggregation to 200 m and 500 m reduced maxima to 58.07 and 53.35 people/km2, respectively. This is consistent with Annex F: finer grids inflate local peaks, whereas coarser grids smooth them. The 200 m grid was therefore selected as the representative scale for intrinsic ground-risk assessment for flights below 500 ft AGL.
The full code, setup instructions, and example outputs are publicly available (https://github.com/GuyMaalouf/opc-worldpop-analysis accessed on 8 January 2026).
c.
Notes on Interpretation:
WorldPop is effective for broad-scale assessments but omits non-resident and transient populations (tourists, mobile staff, temporary workers). In Ol Pejeta, this omission is important near camps or ranger posts that are not reflected in census data. Furthermore, raster values represent averages over grid cells, which can mask strong local clustering.
These limitations, together with grid-size sensitivity, underline the need to combine raster-based estimates with local knowledge and ground observations when deriving exposure values for iGRC analysis.

Appendix B.6. Tabulated Determination of Intrinsic Ground Risk Class (iGRC)

The table below is adapted from Table 8 of the SORA 2.5 main body [9] and is used to determine the intrinsic Ground Risk Class (iGRC) based on estimated population density and aircraft characteristics.
Table A5. Intrinsic Ground Risk Class (iGRC) as a function of population density, UAS characteristic dimension, and maximum speed. Adapted from Table 8 of SORA 2.5 [9]. Highlighted cell shows the classification for our case.
Table A5. Intrinsic Ground Risk Class (iGRC) as a function of population density, UAS characteristic dimension, and maximum speed. Adapted from Table 8 of SORA 2.5 [9]. Highlighted cell shows the classification for our case.
Max UAS Characteristic Dimension1 m3 m8 m20 m40 m
Maximum Speed25 m/s35 m/s75 m/s120 m/s200 m/s
Max population density [ppl/km2]Controlled12345
<523456
<5034567
<50045678
<500056789
<50,000678910
≥50,00078Not part of SORA

Appendix B.7. Fine-Grained Estimation of iGRC Using SORA Annex F

This appendix outlines the full calculation process of the intrinsic Ground Risk Class (iGRC) using the refined method described in Annex F of the SORA. This approach uses physical parameters of the aircraft and the estimated ground population density to compute a continuous risk score.
Annex F defines the iGRC as:
iGRC = 7 + log 10 ( D pop · A C )
where:
  • D pop : population density in people/m2.
Drones 10 00178 i001
  • A C : critical area in m2, representing the ground footprint where an individual might be lethally impacted.
The critical area A C for aircraft with wingspans between 1 m and 8 m (Case 2 in Annex F Section 1.8.2) is calculated as:
A C = 0.6 2 r D ( d glide + d slide ,   reduced ) + π r D 2
Each component is now explained and computed using default values from Annex F as seen in Table A6:
Table A6. Default Parameters from Annex F used in Critical Area Estimation.
Table A6. Default Parameters from Annex F used in Critical Area Estimation.
VariableDescriptionValue
r person Radius of a person0.3 m
h person Height of a person1.8 m
eCoefficient of restitution0.657
θ Impact angle 35
C g Ground friction coefficient0.75
gGravitational acceleration9.8 m/s2
K non - lethal Non-lethal kinetic energy threshold290 J
  • r D : Effective impact radius combines the radius of a person and half the aircraft’s wingspan. This accounts for a lethal area that extends both from the person struck and the size of the aircraft:
    r D = r person + wingspan 2 = 0.3 + 3.8 2 = 2.2   m
  • d glide : Glide distance estimates how far the aircraft can travel horizontally during descent, using the person height as a proxy for impact height:
    d glide = h person tan ( θ ) = 1.8 tan ( 35 ) 2.57   m
  • v horizontal : Horizontal impact velocity, the component of aircraft speed along the ground:
    v horizontal = v · cos ( θ ) = 20 · cos ( 35 ) 16.38   m / s
  • v non - lethal : Non-lethal velocity, the speed below which impact energy is less than K n o n l e t h a l (290 J):
    v non - lethal = 2 K non - lethal m = 2 · 290 2.1 16.62   m / s
  • t safe : Deceleration time, to decelerate from impact to non-lethal speed:
    t safe = e · v horizontal v non - lethal C g · g = 0.657 · 16.38 16.62 0.75 · 9.8 0.79 s
    Since the result is negative, the aircraft is already below the non-lethal threshold upon impact. Thus:
    t safe = 0
  • d slide ,   reduced : Reduced slide distance, representing the distance over which the aircraft continues to slide after initial impact, until it decelerates to a non-lethal velocity:
    d slide ,   reduced = e · v horizontal · t safe 1 2 C g g t slide 2 = 0
    Because t safe = 0 , there is no additional contribution from sliding.
We now compute the final critical area using the full expression:
A C = 0.6 2 r D ( d glide + d slide , reduced ) + π r D 2 = 0.6 2 · 2.2 · ( 2.57 + 0 ) + π · 2 . 2 2 15.91 m 2
Using a population density of 50 people/km2 (converted to 5 · 10 5 people/m2), we find:
D pop = 50 1000000 = 5 · 10 5 people / m 2
Final calculation of iGRC:
iGRC = 7 + log 10 ( D pop · A C ) = 7 + log 10 ( 0.0007955 ) = 7 3.10 = iGRC 4
This example illustrates how the fine-grained Annex F method can yield a lower iGRC compared to Table A5, which places our use case in iGRC 4 instead of iGRC 5. While the tabulated method enables fast and conservative assessments, it may over- or under-estimate the actual risk for borderline cases like ours. The analytical approach of Annex F offers a more accurate evaluation aligned with aircraft specifics.

Appendix B.8. Ground Risk Mitigation Measures (SORA Step 3)

This appendix provides definitions and rules for the ground risk mitigation measures used in Step 3 of the SORA, based on Annex B of the official SORA 2.5 documentation.
Table A7. Summary of Ground Risk Mitigation Measures (Step 3 of the SORA).
Table A7. Summary of Ground Risk Mitigation Measures (Step 3 of the SORA).
MitigationDefinition, Conditions, and Notes
(M1a) Strategic Mitigation by ShelteringApplies when uninvolved people are physically sheltered (e.g., inside vehicles or buildings).
• Integrity: depends on proportion of people sheltered.
• Assurance: depends on confidence in shelter presence and usage.
• Constraint: if claimed at medium robustness, cannot be combined with M1b to avoid double counting.
(M1b) Operational RestrictionsImplements time- or space-based limits to reduce likelihood of overflying people (e.g., avoiding roads, camps, or public areas; restricting times of operation).
• Medium integrity: may be claimed if the at-risk population is reduced by ≥90%.
(M1c) Ground Observation/AwarenessReduces risk by detecting uninvolved people using visual observers, onboard cameras or sensors, or reports from ground staff.
Typically limited to low robustness for BVLOS flights unless supported by automation.
(M2) UAS Impact Energy ReductionApplies when technologies limit impact energy below lethal thresholds, such as parachute systems, frangible structures, or low-energy components.
• Requirement: ground impact energy must be demonstrably non-lethal, typically <290 J.

Appendix B.9. Tactical Mitigation Performance Requirements (Step 6)

Table A8 below reproduces the TMPR criteria defined in Table 1 of Annex D of the SORA 2.5 [9], which establish the minimum performance standards for the detect–decide–command–execute–feedback loop under low robustness conditions (ARC-b). These requirements describe how an operator must detect and respond to unexpected air encounters during flight, ensuring adequate situational awareness, command responsiveness, and descent capability even in the absence of high-integrity systems.
Table A8. Tactical Mitigation Performance Requirements (TMPR) for low robustness (ARC-b) operations, adapted from Table 1 of Annex D in the SORA 2.5 [9].
Table A8. Tactical Mitigation Performance Requirements (TMPR) for low robustness (ARC-b) operations, adapted from Table 1 of Annex D in the SORA 2.5 [9].
Detect
Low (ARC-b)
The expectation is for the applicant’s Detect And Avoid (DAA) plan to enable the operator to detect approximately 50% of all aircraft in the detection volume. This is the performance requirement in absence of failures and defaults. It is required that the applicant has awareness of most of the traffic operating in the area in which the operator intends to fly, by relying on one or more of the following:
  • Use of (web-based) real time aircraft tracking services
  • Use Low Cost ADS-B In / UAT / FLARM / Pilot Aware aircraft trackers
  • Use of UTM Dynamic Geofencing
  • Monitoring aeronautical radio communication (i.e., use of a scanner)
Decide
Low (ARC-b)
The operator must have a documented de-confliction scheme, in which the operator explains which tools or methods will be used for detection and what the criteria are that will be applied for the decision to avoid incoming traffic. In case the remote pilot relies on detection by someone else, the use of phraseology will have to be described as well. Examples:
  • The operator will initiate a rapid descend if traffic is crossing an alert boundary and operating at less than 1000ft.
  • The observer monitoring traffic uses the phrase: ‘DESCEND!, DESCEND!, DESCEND!’.
Command
Low (ARC-b)
The latency of the whole command (C2) link, i.e., the time between the moment that the remote pilot gives the command and the airplane executes the command must not exceed 5 s.
Execute
Low (ARC-b)
UAS descending to an altitude not higher than the nearest trees, buildings or infrastructure or ≤ 60 feet AGL is considered sufficient. The aircraft should be able to descend from its operating altitude to the ‘safe altitude’ in less than a minute.
Feedback loop
Low (ARC-b)
Where electronic means assist the remote pilot in detecting traffic, the information is provided with a latency and update rate for intruder data (e.g., position, speed, altitude, track) that support the decision criteria. For an assumed 3 NM threshold, a 5 s update rate and a latency of 10 s is considered adequate.

Appendix B.10. Platform-Specific Command and Execute Performance (TMPR Analysis)

This section summarises the Command and Execute performance of each platform used during the operation, in relation to the tactical mitigation performance requirements (TMPR) for ARC-b operations. It complements the general overview presented in Table 4 (Step 6) by providing detailed link types, estimated control latency, and descent performance for each platform.
Table A9. Platform-level comparison of Command and Execute performance vs. TMPR (ARC-b).
Table A9. Platform-level comparison of Command and Execute performance vs. TMPR (ARC-b).
PlatformCommand
C2 Link
Command
Latency (ms)
Execute Descent
(120 m → 18 m)
DJI Mavic 3 (E/T [73], P [74])DJI O3/O3+~130 ms [74]6 m/s [73]⇒ ≈17 s
DJI Mavic 2 [75]DJI OcuSync 2.0~130 ms [75]3 m/s [75] ⇒ ≈34 s
DJI Mini 3 Pro [76]DJI OcuSync 2.0~130 ms [76]5 m/s [76] ⇒ ≈20 s
Parrot Anafi [77]Skycontroller 3 (Wi-Fi) [77]≤250 ms [78]4 m/s [77] ⇒ ≈26 s
Codrone Aluco [79]CubePilot Herelink [80]~110 ms [80]3 * m/s ⇒ ≈34 s
Codrone Noctu [79]CubePilot Herelink [80]~110 ms [80]3 * m/s ⇒ ≈34 s
“Papa Smurf” (UoB multirotor)FrSky R-XSR (ACCESS, 2.4 GHz) [81]≤150 ms [82]3 * m/s ⇒ ≈34 s
eBee XProprietary 2.4 GHz ground modem≤150 ms [82]3 * m/s ⇒ ≈34 s
UoB Fixed-Wing Glider (NAN Xplorer [83])FrSky R-XSR (ACCESS, 2.4 GHz) [81]≤150 ms [82]3 * m/s ⇒ ≈34 s
* Estimated value.

Appendix B.11. Determination of the SAIL

The SAIL defines the degree of assurance and integrity required for an operation. It results from the intersection of the final GRC and the residual ARC, as shown in Table A10.
Table A10. Determination of the SAIL, reproduced from the official SORA 2.5 Main Body, Step 7 [9].
Table A10. Determination of the SAIL, reproduced from the official SORA 2.5 Main Body, Step 7 [9].
SAIL Determination
Final GRCARC-aARC-bARC-cARC-d
≤2IIIIVVI
3IIIIIVVI
4IIIIIIIVVI
5IVIVIVVI
6VVVVI
7VIVIVIVI
>7Certified operation

Appendix B.12. Population-Raster Analysis of the Adjacent Area

To determine the containment requirement in SORA Step 8, we evaluated the adjacent area surrounding the conservancy using a top-down population-raster analysis. The adjacent area corresponds to a 5 km ring around the contingency volume (Case A in SORA 2.5 §5.1.3). Our fastest UAS is software-limited to 20 m/s, yielding a maximum displacement of 3.6 km in 3 min. Because this remains below 5 km, the operation falls under Case A, and a conservative 5 km radius was therefore applied (Figure A1).
Population values were extracted from the 2020 WorldPop raster (100 m resolution) and processed using Python scripts for raster clipping, aggregation to 1 km cells, and statistical summarisation of densities within the 5 km ring. All scripts and datasets are available in our public repository (https://github.com/GuyMaalouf/opc-worldpop-analysis accessed on 8 January 2026). Figure A3 illustrates the resulting spatial distribution.
Figure A3. Population density within the 5 km adjacent area surrounding the Ol Pejeta operational volume, derived from WorldPop (2020), at 100 m (left) and 1 km (right) resolutions.
Figure A3. Population density within the 5 km adjacent area surrounding the Ol Pejeta operational volume, derived from WorldPop (2020), at 100 m (left) and 1 km (right) resolutions.
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Clipping the WorldPop raster to the adjacent area produced an average population density of D ¯ p o p = 52.3 ppl / km 2 and a maximum of D p o p , m a x = 900.7 ppl / km 2 at the native 100 m resolution. Aggregating to 1 km cells reduced these values to D ¯ p o p = 43.5 ppl / km 2 and D p o p , m a x = 460.2 ppl / km 2 . This behaviour reflects the grid-size effect described in SORA Annex F and discussed in Section 2.2.4 of the main paper: finer grids highlight isolated single-cell peaks, whereas coarser grids smooth local extremes and better reflect the spatial scale relevant to UAS dispersion.
To remain conservative while avoiding sensitivity to isolated high-density cells, we adopted representative values of D ¯ p o p 50 ppl / km 2 and D p o p , m a x < 500 ppl / km 2 for the adjacent-area assessment. These values align with the refined estimates used in the main paper and support the containment analysis in Step 8.

Appendix B.13. Containment Requirements for 8 m UA (Excerpt from SORA 2.5 Main Body)

The following table reproduces Table 11 from the SORA 2.5 main body [9]. It provides the tabulated containment requirements for unmanned aircraft systems (UAS) with a characteristic dimension of up to 8 m and a cruise speed below 75 m/s. Sheltering is assumed to be not applicable for UAS operating in the adjacent area, and containment levels are expressed as Low, Medium, or High depending on the SAIL and the population exposure characteristics.
Table A11. Containment requirements for 8 m UAS (adapted from SORA 2.5 Main Body, Table 11 [9]).
Table A11. Containment requirements for 8 m UAS (adapted from SORA 2.5 Main Body, Table 11 [9]).
8 m UA (<75 m/s)
Sheltering Assumed not Applicable for the UA in the Adjacent Area
Average Population Density AllowedNo Upper Limit<50,000 ppl/km2<5000 ppl/km2<500 ppl/km2<50 ppl/km2
Outdoor Assemblies Allowed within 1 km of the OPS Volume>400kAssemblies of 40k to 400kAssemblies < 40k
SAIL I & IIOut of scopeOut of scopeHighMediumLow
SAIL IIIOut of scopeOut of scopeMediumLowLow
SAIL IVOut of scopeMediumLowLowLow
SAIL VMediumLowLowLowLow
SAIL VILowLowLowLowLow

Appendix B.14. Fine-Grained Calculation of the Adjacent-Area iGRC

Annex F of SORA 2.5 introduces an analytical, fine-grained method for determining the iGRC of the adjacent area. Unlike the operational area, where the iGRC is derived from the maximum local population density, Annex F explicitly specifies that the adjacent area should use a weighted average population density, since a loss-of-containment event is assumed to have a uniformly distributed probability of occurring anywhere within the 5 km ring.
Following the same formulation presented in Equation (A7) of Appendix B.7, which originates from Annex F of the SORA 2.5 documentation [9], the intrinsic ground-risk class is computed as:
i G R C = 7 + log 10 ( D p o p · A C )
where D p o p is expressed in people/m2 and A C is the critical area (m2) representing the potential lethal-impact footprint.
The critical area is given by Annex F Equation (8):
A C = 0.6 2 r D ( d g l i d e + d s l i d e , reduced ) + π r D 2
with parameters identical to those used in Appendix B.7. Using r D = 2.2 m , d g l i d e = 2.57 m , and d s l i d e , reduced = 0 , we obtain A C 15.9 m 2 . Converting D ¯ p o p = 50 ppl / km 2 to 5.0 × 10 5 ppl / m 2 yields:
i G R C = 7 + log 10 ( 5.0 × 10 5 × 15.9 ) = 7 2.9 = 4
Therefore, the intrinsic ground-risk class for the adjacent area is iGRC 4, derived from the weighted average population density within the 5 km ring.

Appendix B.15. Applicability of Ground-Risk Mitigations in the Adjacent Area

Annex F §5.3 provides additional guidance on which ground-risk mitigations remain valid for excursion scenarios (i.e., when an unmanned aircraft leaves its contingency volume). Only mitigations that continue to function or remain logically applicable during a fly-away may be claimed. Specifically, the following may be considered:
  • M1(a)—Sheltering of people, if it can be generalised across the adjacent area;
  • M1(b)—Time-of-day restrictions (e.g., night operations) that reduce outdoor population exposure; and
  • M2—Passive or frangible design features that limit kinetic energy upon impact.
All other mitigations are not applicable to the adjacent-area assessment:
  • M1(b)—Route- or exposure-based arguments, which apply only to controlled flight paths inside the operational volume;
  • M1(c)—Tactical ground observation, as observers cannot provide coverage for an uncontrolled fly-away; and
  • M2—Active mitigation systems (e.g., parachutes or specific descent manoeuvres), which are assumed to fail in a containment breach.
In the present case, none of the permitted mitigations are applicable:
  • Sheltering cannot be assumed, as the surrounding farmlands are primarily worked outdoors during the day;
  • Time-of-day restrictions are inapplicable, since operations occur both by day and by night; and
  • The employed UAS platforms do not feature sufficient frangible or passive design elements to claim M2 credit.
Consequently, the final ground-risk class remains GRC 4. For a SAIL II operation, Annex F §5.3 and Table 27 [9] specify that a final GRC 4 corresponds to no containment requirement.

Appendix B.16. SORA Containment Requirements (Copy of SORA 2.5 Annex F, Table 27 [9])

Table A12 reproduces Table 27 from SORA 2.5 Annex F [9], showing the containment requirement level as a function of the SAIL in the operational volume and the Adjacent Area Final GRC, where:
  • N: No containment requirement
  • L: Low containment requirement
  • M: Medium containment requirement
  • H: High containment requirement
  • Oos: Out of scope
Table A12. SORA Containment Requirements—adapted from SORA 2.5 Annex F, Table 27 [9].
Table A12. SORA Containment Requirements—adapted from SORA 2.5 Annex F, Table 27 [9].
SAIL in the Operational Volume
Adjacent Area GRCIIIIIIIVVVI
≤3N
4LN
5LLN
6MMLN
7HHMLN
8OosOosOosMLN
9 OosML
10 OosM
11 Oos

Appendix B.17. Operational Safety Objectives (SAIL II Summary)

Table A13 and Table A14 reproduce the set of Operational Safety Objectives (OSOs) applicable to SAIL II operations, as defined in SORA 2.5 Annex E. Each OSO identifies a safety objective that must be demonstrated by the operator with an appropriate level of integrity (safety gain) and assurance (method of proof).
  • Integrity: The strength of the safety gain achieved through compliance with the OSO.
  • Assurance: The confidence level in the operator’s evidence or demonstration of that compliance.
Compliance status is shown using the following colour scheme: Green (Met), Orange (Partially met), and Red (Not met). Inline markers (met, partially met, not met) are used to highlight the corresponding status within the text.
Table A13 and Table A14 summarise all OSOs applicable at SAIL II, indicating the required robustness level and how each objective was addressed in the WildDrone BVLOS framework. OSOs #02, #04, #05, #18, #19, and #24 are excluded here, as they are not applicable at SAIL II and only apply at higher SAIL levels.
Table A13. Operational Safety Objectives (SAIL II) with Compliance Assessment (Adapted from SORA 2.5 Annex E)—Part 1.
Table A13. Operational Safety Objectives (SAIL II) with Compliance Assessment (Adapted from SORA 2.5 Annex E)—Part 1.
OSO TitleRequirement (Integrity & Assurance)Compliance Evaluation
OSO #01 Operator is competent and/or provenIntegrity: The applicant is knowledgeable of the UAS being used and as a minimum has the following relevant operational procedures: checklists, maintenance, training, responsibilities, and associated duties.
Assurance: The elements delineated in the level of integrity are available.
Status: Partially met
The team demonstrated operational knowledge of all UAS and used documented checklists during the campaign. Training, maintenance, and role assignments were implemented but not formally recorded; future iterations will include written procedures and role documentation.
OSO #03 UAS maintained by competent/proven entityIntegrity: The maintenance instructions and requirements are defined, cover applicable designer instructions, and are adhered to. The maintenance staff is competent and authorized to perform maintenance.
Assurance: Criterion #1 (Procedure)—Maintenance instructions are documented, recorded in a maintenance log; and a list of authorized maintenance staff is maintained. Criterion #2 (Training)—A record of qualifications, experience, and training of the maintenance staff is maintained.
Status: Not met
No formal maintenance structure exists. There are no documented maintenance instructions, no dedicated maintenance personnel, and no maintenance log or record-keeping system. Maintenance procedures, staff responsibilities, and training records will be established before future operations.
OSO #06 C3 link characteristics (e.g., performance, spectrum use) are appropriate for the operationIntegrity: The applicant determines that performance, RF spectrum usage, and environmental conditions for C3 links (Command and Control (C2), and communication link required for the safety) are adequate to safely conduct the intended operation. The remote pilot has the means to continuously monitor C3 performance and ensure it continues to meet operational requirements.
Assurance: The applicant declares that the required level of integrity has been achieved.
Status: Met
All UAS operated on 2.4 GHz with some equipped for dual-band (2.4/5.8 GHz) operation, within authorized ISM bands. C2 link performance was continuously monitored through RSSI values during pre-flight and in-flight phases. Custom-built platforms (relying on 2.4 GHz FrSky ACCESS protocol) provided equivalent monitoring capability. Additional VHF and local radio communications were used for situational awareness and coordination with Ol Pejeta radio control, but their reliability was not quantitatively verified. Overall, the C3 systems provided sufficient robustness for the operational context.
OSO #07 Conformity check of the UAS configurationIntegrity: The Operator has UAS conformity check procedures ensuring that the aircraft used is in a safe condition and that its configuration conforms to the design data and operational limitations considered under the approved concept of operations.
Assurance: Documented conformity check procedures exist and reflect the designer’s recommendations. The remote crew is trained to perform conformity checks.
Status: Partially met
No modifications were made to any UAS, and all platforms matched the configurations described in the application, ensuring conformance in practice. However, no formal conformity check procedure or training was implemented. Future operations will include a documented conformity verification and corresponding crew training.
OSO #08 Operational procedures defined, validated, adhered toIntegrity: Appropriate operational procedures are defined and cover flight planning; pre-/post-flight inspections; evaluation of environmental conditions; normal, contingency, and emergency procedures; pre-flight briefing of involved persons; occurrence reporting; and ERP.
Assurance: Procedures are developed to standards acceptable to the competent authority; adequacy of contingency/emergency procedures is proven via dedicated flight tests or validated simulation (FTB alternative not used).
Status: Partially met
Procedures covered flight planning, pre-/post-flight inspections, environmental evaluation, and normal, contingency, and emergency procedures, with radio coordination and human-error mitigation. Occurrence reporting was limited to a post-flight note, and no dedicated Emergency Response Plan (ERP) addressing secondary effects existed. Contingency and emergency simulations were conducted during training, but procedures were not aligned with a recognised standard, and total flight hours insufficient for a functional test-based assurance claim.
Table A14. Operational Safety Objectives (SAIL II) with Compliance Assessment (Adapted from SORA 2.5 Annex E)—Part 2.
Table A14. Operational Safety Objectives (SAIL II) with Compliance Assessment (Adapted from SORA 2.5 Annex E)—Part 2.
OSO TitleRequirement (Integrity & Assurance)Compliance Evaluation
OSO #09 Remote crew trained and currentIntegrity: Theoretical and practical training ensures knowledge of UAS regulation, airspace principles, airmanship and aviation safety, human performance limitations, meteorology, navigation, UAS knowledge, operational procedures and ERP, and use of external services. Training must enable the remote crew to manage normal, abnormal, and emergency situations resulting from technical issues, human errors, or environmental conditions, and must define proficiency and training recurrence.
Assurance: Training is self-declared, with supporting evidence available on request.
Status: Partially met
The remote crew underwent theoretical and practical training focused on operational procedures and safety, including pre-flight, contingency, and emergency actions. However, several areas were only partially addressed or omitted: UAS regulations, airspace principles, airmanship, human performance, navigation, and use of external services. No formal proficiency or recurrence requirements were defined. Future training cycles will expand coverage to all competency areas and include defined refresh intervals.
OSO #13 External servicessupporting UASoperations areadequate to the operationIntegrity: The applicant ensures that the level of performance for any externally provided service critical to the safety of flight is adequate for the intended operation. Where communication with a Service Provider is required, effective coordination and defined responsibilities must be in place.
Assurance: The applicant declares that the requested level of performance for any externally provided service necessary for flight safety is achieved, with supporting evidence available upon request.
Status: Met
The operation relied solely on Global Navigation Satellite System (GNSS) positioning as an external service. GNSS performance was adequate, with the number of satellites monitored before and during each flight, and failsafes in place to manage GPS loss. No other external service providers (e.g., CSP, UTM, power) were used, and all critical functions were managed internally with built-in failsafes.
OSO #16 Multi-crew coordinationIntegrity: Procedure(s) ensure coordination between crew members with robust, effective communications covering: task assignment and step-by-step communications with proper phraseology.
Assurance: Procedures do not need to be validated to a formal standard; adequacy is declared. Remote-crew training on multi-crew coordination is self-declared.
Status: Met
Operations with multiple UASs used co-located pilots with direct voice comms, takeoff/landing coordination, and vertical separation. Extended BVLOS remote observers employed internet audio, defined call-signs and read-backs (“Pilot/Observer… over”), brevity codes (e.g., Intruder, Kill Kill Kill, Down down down) and message types (Information/Warning/Alert). Communications were tested pre-flight.
OSO #17 Remote crew is fit to operateIntegrity: The applicant defines how crew declare fitness before duty and report unfitness during operations, considering fatigue, stress, substance use, and environmental factors.
Assurance: The policy and declaration process are documented.
Status: Met
The pre-flight procedure verified Remote crew fitness through the IMSAFE checklist(Illness, Medication, Stress, Alcohol, Fatigue, Emotion). Packing checklist included PPE appropriate to conditions (e.g., hats, mosquito repellent, headlamps, jackets). A written policy on duty and rest periods will be formalized.
OSO #20 A Human Factors evaluation has been performed and the Human-Machine Interface (HMI) found appropriate for the missionIntegrity: UAS information and controls are clearly presented and do not confuse, cause unreasonable fatigue, or contribute to crew error. If an electronic aid is used to maintain UA awareness, its HMI allows position determination and does not degrade visual scanning or crew communications.
Assurance: A human factors evaluation is conducted (by inspection/analysis) to determine suitability for the mission; adequacy of the result is declared or validated through simulation (FTB alternative not used).
Status: Partially met
Operations employed COTS HMIs (with map/telemetry on handheld displays) and QGroundControl & ArduPilot for custom platforms; these provided clear UA state/position without impeding visual scanning or radio comms. However, no formal human factors evaluation (documented inspection/analysis with declared adequacy) was performed; informal usability checks occurred but were not recorded to a recognised method.
OSO #23 Environmental conditions for safe operations defined, measurable, and adhered toIntegrity: Environmental conditions for safe operations are defined and reflected in the flight manual or equivalent document.
Assurance: The applicant declares that the required level of integrity has been achieved.
Status: Met
Operational procedures defined limits for temperature (−10 °C to 40 °C), wind speed (<10 m/s), precipitation (up to light drizzle), visibility (>5 km), and Kp-index (≤5). These limits were verified during planning and pre-flight using forecasts and on-site assessment.

Appendix C. Field Trial Cards—Operational Insights from Real-World Operations

This appendix compiles a series of Field Trial Cards summarising key missions conducted during the WildDrone operations in Kenya. Each card presents a concise account of a specific field activity, outlining its objective and mission context, operational summary and procedures, and the main challenges and lessons learned. Together, these records capture the diversity of experimental objectives and illustrate how practical field experience informed the continuous refinement of our operational framework. The cards provide both a technical and procedural overview of how research missions were planned and executed under real-world conditions, serving as a reference for future large-scale conservation operations and regulatory studies.
Table A15. Field Trial Card #1—Night Tracking of Lions to Study Predator Behaviour.
Table A15. Field Trial Card #1—Night Tracking of Lions to Study Predator Behaviour.
Objective & Mission ContextThe mission aimed to track a lion pride (Panthera leo) during peak nocturnal activity to study movement patterns and hunting strategies in relation to prey distribution. Prides of up to 20 individuals were first located using VHF-GPS collars on dominant females and then monitored across different habitats, from open grasslands to dense bushland.
Operational SummaryNight tracking was conducted over 58 nights (during an extended fieldwork period following the WildDrone hackathon), with up to 10 flights per night between 7 pm and 3 am using a DJI Mavic 3 Enterprise Thermal. Two safety incidents occurred: (i) an emergency rooftop recovery due to the proximity of lions, and (ii) a mission aborted following the unexpected landing of an unlit aircraft near the operational area, within airspace previously confirmed as inactive for nighttime activity.
Operational ProceduresNight operations during the extended conservation fieldwork period were conducted by a three-person crew, with the copilot also serving as airspace observer and a ranger equipped with a firearm ensuring ground safety. All flights were operated from within the vehicle to mitigate wildlife risk. Missions remained below 400 ft AGL west and 250 ft AGL east of the Ewaso River, and within 1 km (BVLOS) from the pilot. Following a safety assessment and coordination with Ol Pejeta Conservancy management and KAF ATC, the nighttime restriction around Kamok Airstrip was lifted to permit controlled operations in that sector, enabling continued tracking of a key lion pride while maintaining verified airspace safety.
Operational Challenges & LessonsPredator activity increases ground risk: Night operations required a modified crew setup, with all missions flown from within the vehicle and a ranger equipped with a firearm ensuring ground safety. This configuration was required as predators are more active and less visible at night.  
Vehicle-based flying requires adaptations: Conducting flights from a vehicle roof reduced exposure to wildlife but limited upward visibility for air risk assessment. Using open-roof field vehicles provided an effective balance between crew protection and situational awareness.  
Night conditions require audio logging: Mounting a head-mounted GoPro for safety documentation, as per our procedures, proved impractical at night, as it conflicted with the use of a head torch and captured no usable footage in darkness. Continuous audio logging was therefore adopted as a practical alternative for post-flight safety review.  
Fatigue management at night becomes essential: IMSAFE crew assessments were repeated before, after, and between missions, with special focus on fatigue due to the physically demanding nature of night operations.  
Fixed home point limits efficiency: In accordance with our procedures, the Return to Home (RTH) position remained static while tracking moving lions, preventing vehicle repositioning during flight. This constraint led to longer transit times and battery use, whereas a dynamic RTH would have improved efficiency and mission continuity.
Table A16. Field Trial Card #2—Evaluating a UAS Swarm System for Multi-Perspective Data Collection.
Table A16. Field Trial Card #2—Evaluating a UAS Swarm System for Multi-Perspective Data Collection.
Objective & Mission ContextTo evaluate a drone swarm framework for coordinated, autonomous, multi-perspective monitoring of Plains zebras (Equus quagga). The mission validated a centralised particle swarm optimisation controller that autonomously assigned waypoints to multiple drones to achieve optimal visual coverage while minimising disturbance to the animals. Field experiments targeted herds of 20–50 individuals in open grasslands with scattered bushes. The ground station and crew had to remain at least 200 m from the animals to avoid disturbance and behavioural interference. Full details are available in the following studies [22,23,24].
Operational SummaryAcross 6 days, 12 successful missions were flown under variable wind conditions using 3 Commercial Off The Shelf (COTS) drones (2x DJI Mini 3 and 1x DJI Mavic 3E). No safety incidents or loss of link were recorded during any operation.
Operational ProceduresFlights were conducted under VLOS rules, with one pilot per drone. A minimum vertical separation of 15 m was maintained to prevent mid-air collisions.
Operational Challenges & LessonsLarge teams reduce scalability: The one-pilot-per-drone requirement demanded a large team, limiting scalability and increasing logistical complexity. Allowing a single qualified pilot to manage multiple drones would make such operations more scalable for real-world deployment.
Short range limits observation time: The VLOS range constrained the observable area and imposed time pressure as herds moved beyond the effective control radius. Extending this range would ease the limitation and allow longer data-collection windows.
Vertical spacing limits fleet size: A 15 m vertical separation ensured safe spacing for the 3-drone configuration but limits the operation to a maximum of 8 drones that can safely operate within the 120 m altitude ceiling. Reducing this spacing could enable more drones to operate within the same airspace while maintaining safety margins.
Procedural refinement boosts efficiency: Setup time decreased from roughly 30 min to 10 min as the crew became familiar with their roles and implemented parallel pre-flight tasks, highlighting how procedural refinement and targeted training enhance efficiency.
Table A17. Field Trial Card #3—Assessing Wildlife Behavioural Response to Drone Approaches.
Table A17. Field Trial Card #3—Assessing Wildlife Behavioural Response to Drone Approaches.
Objective & Mission ContextThe mission investigated the behavioural responses of wildlife to drone approaches under varying conditions, with the goal of assessing tolerance and vigilance across environmental contexts. Field trials targeted herds of plains zebras (Equus quagga) in open grasslands, with the crew required to remain at least 200 m from the animals to avoid disturbance.
Operational SummaryData was collected using horizontal approaches at controlled speed and a constant altitude of 165 ft (50 m) AGL. A total of 32 successful missions were conducted over 8 days (during an extended conservation fieldwork period following the WildDrone hackathon) using a DJI Mavic 3T for short flights of 5–10 min. All missions took place during daytime under variable wind conditions. No safety incidents or technical malfunctions occurred, and all operations complied with local regulations.
Operational ProceduresDuring the extended fieldwork phase, the copilot and airspace observer roles were combined to enable a three-person crew configuration. Flights were conducted below 250 ft AGL and within VLOS from the pilot, aligning operational procedures with the needs of long-duration biological missions.
Operational Challenges & LessonsPre-flight setup minimises disturbance: Pre-flight tasks were executed carefully to reduce animal disturbance, with the crew remaining inside vehicles whenever possible. Limited visibility from closed roofs constrained air risk assessment and was mitigated by using open-roof field vehicles.  
Procedures training improves efficiency: Training team members and performing setup tasks in parallel reduced preparation time from 20 to 10 min, decreasing animal disturbance and the likelihood of herds moving beyond VLOS limits, which would disrupt operations. 
Fixed home point limits flexibility: A static home point complicated operations when animals moved after initial approaches, occasionally pushing them beyond VLOS range and requiring in-field adjustments.
Table A18. Field Trial Card #4—Drone-Based Data Collection for Individual Rhino Identification.
Table A18. Field Trial Card #4—Drone-Based Data Collection for Individual Rhino Identification.
Objective & Mission ContextThe mission aimed to collect aerial footage of Black and White rhinos (Diceros bicornis and Ceratotherium simum) for photogrammetric assessment and to train a computer vision algorithm for individual recognition. These data support conservation authorities in monitoring age, sex, health, and reproductive status across the population. Ultimately, the work seeks to provide ranger teams with practical drone-based tools that automate daily monitoring and reduce the need for dangerous foot patrols in the bush. Flights targeted small groups during daytime across habitats ranging from open grassland to dense bush, with the crew maintaining a 200 m distance to minimise disturbance and ensure safety.
Operational SummaryAcross 24 days (during an extended conservation fieldwork period following the WildDrone hackathon), the team conducted 93 flights totalling 21 h using a DJI Mavic 3 Pro equipped with a downward-facing laser rangefinder (https://www.o3st.com/index.php/o3st-products/, accessed on 29 January 2026) to refine altitude measurements for photogrammetry. Apart from one mission interrupted due to the pilot feeling unwell, no safety incidents or loss of link occurred throughout the campaign.
Operational ProceduresDuring the extended fieldwork phase, the copilot and airspace observer roles were combined to enable a three-person crew configuration. This adjustment was balanced by reducing the maximum flight envelope to 250 ft AGL and 1 km (BVLOS), better matching staffing constraints and reducing operational overhead during extended fieldwork.
Operational Challenges & LessonsCompact crew enhances flexibility: The three-person configuration functioned effectively in practice. The operator managing both copilot and airspace observation tasks did not report excessive workload or stress, and the smaller crew structure improved flexibility and reduced logistical demands, benefits that are valuable for extended conservation fieldwork.  
Low-altitude disturbs wildlife: The 250 ft ceiling was restrictive, as rhinos were sensitive to drone noise at lower altitudes. Operating higher would allow monitoring with less disturbance and reduced risk of aggression.  
Range limits operational potential: The 1 km BVLOS range was sufficient for the data-collection phase supporting algorithm development, but future autonomous census and identification missions will require longer-range capability to fully unlock this potential.  
Exclusion zones hinder monitoring: Restrictions around designated areas significantly limited coverage, excluding several rhino territories and thus creating major data gaps, requiring riskier, more labour-intensive, and less comprehensive ground surveys.  
Co-developed procedures improve efficiency: The initial checklist, developed by the safety team, was not fully optimised for the rapid, repeated flights typical of fieldwork. Refining its structure based on biologist feedback improved usability and maintained compliance, highlighting the importance of co-developing procedures that balance rigour with practicality.  
Crew training ensures readiness: When a pilot became unwell mid-flight, clear task allocation and adherence to established contingency procedures enabled a safe and coordinated mission termination, highlighting the effectiveness of crew training and readiness to manage in-flight contingencies.
Table A19. Field Trial Card #5—3D Reconstruction and Semantic Segmentation of Natural Habitats.
Table A19. Field Trial Card #5—3D Reconstruction and Semantic Segmentation of Natural Habitats.
Objective & Mission ContextThe mission aimed to generate high-resolution 3D reconstructions of savanna landscapes featuring trees, shrubs, waterholes, and grassland mosaics for semantic segmentation and habitat modelling. These sites represented biodiversity hotspots where vegetation complexity and wildlife presence required ethical operation planning to minimise disturbance and preserve ecological integrity.
Operational SummaryMapping operations were conducted over 4 days using DJI Mavic 3 Pro and DJI Mavic 3 Thermal platforms. Missions required optimal environmental conditions with stable light, moderate temperature, and low wind to ensure photogrammetric accuracy. No safety incidents, communication losses, or equipment malfunctions occurred throughout the campaign.
Operational ProceduresFlights were conducted under BVLOS procedures within 1 km of the pilot, although most operations remained within visual range. The crew consisted of four members—pilot, copilot, air observer, and ground observer. Altitude and lateral distance from vegetation were continuously adjusted to maintain safe clearance and capture complete terrain coverage.
Operational Challenges & LessonsDense vegetation increases collision risk: Flying near trees and shrubs occasionally triggered onboard obstacle sensors and interrupted flight paths. Operating in complex habitats therefore requires refined obstacle-avoidance settings and pre-planned safety corridors.  
Bushland proximity heightens wildlife risk: In dense vegetation, wildlife detection was more difficult, requiring careful pre-flight observation from within vehicles before deployment to ensure safe crew positioning and minimise disturbance.  
Experience improves operational workflow: Setup and checklist times decreased significantly as the crew refined task allocation and coordination, demonstrating how repetition and field experience enhance procedural efficiency.
Table A20. Field Trial Card #6—Testing Collaborative Multi-Agent Aerial Mapping for Wildlife Surveys.
Table A20. Field Trial Card #6—Testing Collaborative Multi-Agent Aerial Mapping for Wildlife Surveys.
Objective & Mission ContextThe mission aimed to extend collaborative multi-UAS mapping research in savanna environments [25] by collecting datasets under realistic wildlife survey conditions. The objective was to evaluate the robustness of collaborative SLAM frameworks when faced with dynamic outdoor scenes and natural variability in illumination, texture, and animal presence. Waypoint missions were used to ensure consistent coverage and sufficient viewpoint overlap between drones for 3D reconstruction and map fusion. Field operations targeted open grasslands with scattered vegetation and active wildlife, conducted during daytime under typical survey conditions.
Operational SummaryThe mission took place over 4 days and consisted of 6 flights using a DJI Mavic 3E and a DJI Mavic 3T operated simultaneously. 4 missions followed waypoint trajectories, while 2 were manually piloted to test flexibility in data acquisition. No safety incidents or equipment malfunctions occurred throughout the campaign.
Operational ProceduresFlights were conducted under VLOS conditions. Each aircraft was operated by a pilot–copilot pair, supported by a shared airspace observer and ground observer. A minimum vertical separation of 10 m was maintained between drones, and take-off and landing were coordinated verbally between pilots positioned side by side to prevent collisions and maintain visual awareness.
Operational Challenges & LessonsSafety protocols limit crew scalability: Current safety requirements demand large teams, typically six for dual-drone missions, placing significant resource constraints on extended deployments. Developing procedures that maintain safety while reducing crew size would improve scalability and long-term feasibility of collaborative mapping operations.  
Crew continuity improves procedural learning: Varying team composition between missions prevented the development of procedural familiarity. Consistent crew assignment would enhance coordination, reduce setup time, and improve efficiency during collaborative flight operations.
Table A21. Field Trial Card #7—Testing Edge-AI Drone Systems for Autonomous Wildlife Monitoring.
Table A21. Field Trial Card #7—Testing Edge-AI Drone Systems for Autonomous Wildlife Monitoring.
Objective & Mission ContextThe mission aimed to field-test two edge-AI-enabled drone systems, WildWing [26] and WildLive [27], developed to advance autonomous wildlife monitoring through onboard perception and tracking. WildWing autonomously tracked animal groups using computer vision models optimised for edge devices, while WildLive performed near real-time detection and tracking of multiple species through onboard inference. Both systems targeted plains zebras, elephants, and giraffes in semi-open savanna habitats. Flights followed ethical distance constraints (≥200 m from animals) and altitudes of 100–265 ft AGL. Field experience from these deployments later informed the development of the MMLA dataset [28], used to improve model generalisation across species and environments.
Operational SummaryThe field campaign spanned 5 days, comprising 10 missions: 4 WildWing flights and 6 WildLive flights. The WildWing system used a Parrot Anafi controlled from a GPU-equipped ground station running custom autonomous tracking software. The WildLive system employed the Papa Smurf quadcopter, a custom-built platform equipped with an onboard NVIDIA Jetson Nano for real-time detection and manual piloting. All operations were conducted in daylight with clear skies, moderate temperatures, and little wind, and completed without safety incidents or equipment malfunctions.
Operational ProceduresFlights were conducted under VLOS conditions. Each aircraft was operated by a pilot–copilot pair, supported by an airspace observer and ground observer. The crew maintained a minimum 200 m distance from animals and adapted flight altitudes (100–265 ft AGL) to reduce disturbance while maintaining tracking performance.
Operational Challenges & LessonsCustom platforms require adaptation: Integrating bespoke hardware and software in the field introduced reliability and setup challenges, particularly when systems behaved differently from laboratory tests. Early on-site validation and modular designs are key to streamlining field readiness for complex AI-driven platforms.  
Standardised procedures enable quick adaptation: Using the standardised checklists and communication protocols prepared for the WildDrone hackathon helped bring team members up to speed quickly, ensuring consistent performance among mixed-experience operators and maintaining high operational safety throughout the deployment.
Table A22. Field Trial Card #8—Assessing Multi-Object Tracking for Wildlife Monitoring.
Table A22. Field Trial Card #8—Assessing Multi-Object Tracking for Wildlife Monitoring.
Objective & Mission ContextThe mission aimed to evaluate the WildLive multi-object tracking framework [27] designed to identify and track multiple animal species in real-world field conditions. Tests focused on zebras, giraffes, and elephants, both as individuals and in herds of 5–20 animals across open grasslands with scattered bushes. The trials validated the system’s performance in live scenarios and contributed to a growing dataset supporting automated wildlife detection [28]. Flights were carried out using a custom quadcopter platform equipped with a Jetson AGX Orin computer for onboard processing.
Operational SummaryAcross 2 days, a total of 6 missions were conducted, each lasting approximately 15 min. Flights were performed at altitudes between 165 ft (50 m) and 400 ft (120 m) AGL, with a minimum altitude of 50 m maintained to reduce noise disturbance from the custom platform. All missions were flown during daytime under sunny, stable conditions, and completed without safety incidents or technical malfunctions.
Operational ProceduresOperations were conducted under BVLOS procedures within a 1 km radius. The crew consisted of four members: a pilot, copilot, airspace observer, and ground observer. Each flight followed the approved checklists and communication protocols established for the WildDrone field campaign, ensuring consistent compliance and coordinated mission execution.
Operational Challenges & LessonsHigher altitude reduces tracking accuracy: A 50 m minimum flight altitude was maintained to limit animal disturbance from drone noise. This constraint led to reduced detection and tracking precision, highlighting the trade-off between animal welfare and algorithmic performance in field deployments.
Table A23. Field Trial Card #9—Assessing Behavioural Responses of Wildlife to Drone Noise.
Table A23. Field Trial Card #9—Assessing Behavioural Responses of Wildlife to Drone Noise.
Objective & Mission ContextThe mission aimed to quantify how drone-generated noise affects the behaviour of large African herbivores under realistic field conditions. Trials focused on plains zebras (Equus quagga) and reticulated giraffes (Giraffa reticulata) at Ol Pejeta Conservancy, integrating in-situ acoustic measurements with standardised behavioural scoring. The broader goal was to determine species-specific disturbance thresholds and support the development of ethical, evidence-based guidelines for wildlife monitoring using drones [29,30].
Operational SummaryAcross 4 days, a total of 13 flight trials were conducted using DJI Mavic 3 Pro and DJI Mavic 3 Thermal platforms. Flights were performed at altitudes between 65 ft (20 m) and 250 ft (75 m) AGL, following a standardised profile: a vertical ascent, a horizontal approach at 3–5 m/s, a 60 s hover, and a return along the same trajectory. Dual-drone missions were carried to assess additive acoustic effects. A calibrated ground microphone array, spaced at 5 m intervals parallel to the flight path, recorded broadband noise, while trained observers logged animal behaviour in real time using an ethogram. Flights were launched at least 500 m away from the animals to minimise pre-exposure disturbance. All operations were completed safely with no incidents or equipment malfunctions.
Operational ProceduresFlights were conducted under BVLOS procedures within a 1 km operational radius. Crew composition included a pilot and copilot per drone, as well as a shared airspace observer and ground observer, and behavioural monitors coordinating via radio to ensure animal welfare. For dual-drone operations, pilots coordinated take-off and landing verbally while maintaining 10 m vertical separation to prevent mid-air conflicts. Real-time communication between flight and behavioural teams ensured rapid response if distress behaviours occurred.
Operational Challenges & LessonsLarge crews reduce scalability: Dual-drone operations under BVLOS procedures required up to six team members (2 pilots, 2 copilots, and 2 shared safety observers), making such missions resource-intensive and less scalable for repeated deployments. Managing multiple personnel increases coordination demands and planning complexity.
Dual-UAS coordination increases workload: Maintaining vertical separation, synchronising timing, and communicating between both aircraft and ground teams added significant procedural overhead. Balancing the experiment’s data-collection needs with safety monitoring made real-time coordination challenging and occasionally reduced operational flexibility.
Safety procedures slow mission turnover: Pre-flight documentation and stepwise approvals ensured safety and compliance but limited the ability to conduct quick successive missions. The thoroughness of these processes improved safety assurance but reduced overall efficiency and data throughput.
Range limits operational coverage: The 1 km BVLOS range, combined with the required 500 m launch distance from animals, left a narrow 500 m operational window. As herds moved beyond this area, flights had to be terminated and the crew repositioned, reducing observation time and increasing setup requirements.
Crew training improves efficiency: Crew training and the use of standardised procedures helped offset delays by improving setup speed, data consistency, and overall workflow efficiency across repeated missions.
Table A24. Field Trial Card #10—Geolocation Accuracy of Animal Positioning using COTS Drones.
Table A24. Field Trial Card #10—Geolocation Accuracy of Animal Positioning using COTS Drones.
Objective & Mission ContextThe mission quantified the geolocation accuracy achievable with COTS drones for animal localisation and size estimation using a monoplotting algorithm. Field experiments examined how positional and size-estimation errors vary with drone altitude and distance. Trials targeted herds of 3–20 plains zebras (Equus quagga) in open savanna with low terrain relief, maintaining at least 100 m separation and altitudes below 280 ft (85 m) to minimise disturbance. Data were collected using one autonomous drone executing waypoint missions and a second manually piloted drone acquiring nadir reference imagery for ground-truth validation [31,32].
Operational SummaryAcross 5 days, 12 missions were flown with 2 COTS platforms (DJI Mavic 3 Thermal and DJI Mini 3). Weather remained clear and dry with variable winds. No safety incidents or loss of link occurred.
Operational ProceduresFlights followed VLOS procedures with one pilot and co-pilot per drone, supported by a shared airspace observer and ground-risk observer. During dual-drone missions, a minimum 15 m vertical separation was maintained for safe coordination.
Operational Challenges & LessonsCrew optimisation improves efficiency: Refining procedures to match the low workload allowed a single copilot to support multiple pilots, reducing the ground crew to five without affecting safety and improving coordination.
Routine operations risk complacency: Although no incidents occurred, the repetitive nature of autonomous missions occasionally reduced vigilance. Consistent cross-checks and situational awareness remain essential during routine or lowworkload flights.
Emergency training strengthens confidence: Additional rehearsal of contingency and emergency procedures would improve crew confidence during unexpected events. Regular scenario-based training is recommended to maintain preparedness.
Table A25. Field Trial Card #11—Stereo vision payload for measurement of animal body condition.
Table A25. Field Trial Card #11—Stereo vision payload for measurement of animal body condition.
Objective & Mission ContextStereo-vision mission using a drone-mounted dual-camera prototype designed to enable non-invasive, metric assessment of animal body condition. Field experiments targeted both herds and solitary animals across plains and sparsely vegetated grasslands.
Operational Summary17 missions were flown with the CoDrone Aluco carrying a custom stereo-vision payload to evaluate its suitability for wildlife monitoring. Three safety incidents occurred:
Unannounced aircraft approach: The airspace observer spotted an approaching aircraft. The contingency procedure was followed: the drone was lowered and returned home for a low-altitude landing.
Geo-fence breach: On reaching the 500 m geo-fence, the drone drifted slightly beyond the boundary. The automatic return behaviour was not fully anticipated, requiring brief manual correction. The total excursion was ∼60 m before control was restored and the mission continued safely.
Battery cover detachment: During take-off, the magnetic battery cover detached due to adhesive failure. The drone was landed immediately, the cover retrieved, and an additional attachment method implemented before further flights.
Operational ProceduresFlights were conducted under VLOS with a single drone operating inside the designated airspace. The crew consisted of four members (pilot, copilot, airspace observer, ground observer), and all WildDrone campaign procedures were followed.
Operational Challenges & LessonsLimited qualified pilots reduce flexibility: Few team members were qualified to fly this platform, reducing crew interchangeability and slowing mission turnover.
Heavy platform reduces agility: The combined drone–payload mass reduced manoeuvrability, slowing evasive and emergency actions. This constraint should be considered when planning operations with heavier systems.
Short range limits observation capacity: Restricted VLOS range and additional setup time for the custom payload increased time pressure and raised the likelihood that animals moved outside the observation area. Extending range would improve coverage.
Procedural refinement improves efficiency: Setup time decreased as the crew gained familiarity with assembly and pre-flight routines, reaching an efficient workflow by the end of the missions.

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Figure 1. SORA semantic map of the January 2025 field campaign. The map visualises the spatial volumes defined in SORA Step 2 to model risk containment: (1) Flight geography (green), the nominal operating area; (2) Contingency volume (orange), set by a 1.5 km horizontal buffer representing a 50 s reaction window at 30 m/s for the fastest UAS; (3) Ground-risk buffer (red), a 400 ft (120 m) band, aligned with the maximum flight altitude, reflecting the ballistic descent footprint used for iGRC determination; (4) Containment area (purple), a 1 km band beyond the ground-risk buffer used in Step 8 to verify containment and identify outdoor assemblies; (5) Adjacent area (light blue), regions outside the containment area where uninvolved people may still be exposed in failure scenarios; (6) Air-risk buffer zones (ruby red), lateral and vertical separation distances from crewed aviation activities based on the maximum UAS altitude; (7) Campgrounds (yellow), treated as sensitive zones and excluded from the operational volume during ground-risk mitigation.
Figure 1. SORA semantic map of the January 2025 field campaign. The map visualises the spatial volumes defined in SORA Step 2 to model risk containment: (1) Flight geography (green), the nominal operating area; (2) Contingency volume (orange), set by a 1.5 km horizontal buffer representing a 50 s reaction window at 30 m/s for the fastest UAS; (3) Ground-risk buffer (red), a 400 ft (120 m) band, aligned with the maximum flight altitude, reflecting the ballistic descent footprint used for iGRC determination; (4) Containment area (purple), a 1 km band beyond the ground-risk buffer used in Step 8 to verify containment and identify outdoor assemblies; (5) Adjacent area (light blue), regions outside the containment area where uninvolved people may still be exposed in failure scenarios; (6) Air-risk buffer zones (ruby red), lateral and vertical separation distances from crewed aviation activities based on the maximum UAS altitude; (7) Campgrounds (yellow), treated as sensitive zones and excluded from the operational volume during ground-risk mitigation.
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Figure 2. Projected annual tourist visits to Ol Pejeta Conservancy for 2016–2025. Blue markers show observed visitor numbers from official conservancy reports [19]. Shaded region highlights COVID-19 downturn from 2019–2021. Projections from 2023 onward combine United Nations World Tourism Organization (UN Tourism) regional recovery rates [17,18] with a pre-pandemic local growth trend of 7%. The central line represents the mid-range estimate, with upper and lower bounds indicating the uncertainty of recovery trajectories.
Figure 2. Projected annual tourist visits to Ol Pejeta Conservancy for 2016–2025. Blue markers show observed visitor numbers from official conservancy reports [19]. Shaded region highlights COVID-19 downturn from 2019–2021. Projections from 2023 onward combine United Nations World Tourism Organization (UN Tourism) regional recovery rates [17,18] with a pre-pandemic local growth trend of 7%. The central line represents the mid-range estimate, with upper and lower bounds indicating the uncertainty of recovery trajectories.
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Figure 3. Estimated population densities within Ol Pejeta Conservancy derived from WorldPop 2020, illustrating the effect of grid resolution on peak density estimates. At 100 m resolution, finer grids produce localised peaks with a maximum of 105 ppl/km2, while aggregation to 200 m and 500 m smooths these variations, reducing maxima to 58 and 53 ppl/km2, respectively. Annex F of the SORA recommends selecting a grid size comparable to the UAS dispersion area (≈200 m below 500 ft AGL).
Figure 3. Estimated population densities within Ol Pejeta Conservancy derived from WorldPop 2020, illustrating the effect of grid resolution on peak density estimates. At 100 m resolution, finer grids produce localised peaks with a maximum of 105 ppl/km2, while aggregation to 200 m and 500 m smooths these variations, reducing maxima to 58 and 53 ppl/km2, respectively. Annex F of the SORA recommends selecting a grid size comparable to the UAS dispersion area (≈200 m below 500 ft AGL).
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Figure 4. Distribution of residential population densities across the operational area using WorldPop 2020 at 100 m resolution. Dashed lines indicate the mean, median, 99th-percentile, and maximum densities (12, 10, 37, 105 ppl/km2, respectively). This highlights the influence of isolated extremes during ground-risk assessments.
Figure 4. Distribution of residential population densities across the operational area using WorldPop 2020 at 100 m resolution. Dashed lines indicate the mean, median, 99th-percentile, and maximum densities (12, 10, 37, 105 ppl/km2, respectively). This highlights the influence of isolated extremes during ground-risk assessments.
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Figure 5. Daily visitor composition in Ol Pejeta Conservancy (25 January–2 February 2025). Stacked bars show overnight and day-trip visitors recorded during the campaign period. The data reveal a stable baseline with occasional surges, including a peak on 31 January driven primarily by day visitors.
Figure 5. Daily visitor composition in Ol Pejeta Conservancy (25 January–2 February 2025). Stacked bars show overnight and day-trip visitors recorded during the campaign period. The data reveal a stable baseline with occasional surges, including a peak on 31 January driven primarily by day visitors.
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Figure 6. Daily visitor counts by camp (25 January–2 February 2025). Box plots summarise visitor distributions at each camp. Most sites show low, tightly clustered counts, while Sweetwaters Tented Camp emerges as a clear hotspot with substantially higher occupancy and a marked outlier (≈208 visitors), illustrating how localised peaks are not captured by raster-based or conservancy-wide averages.
Figure 6. Daily visitor counts by camp (25 January–2 February 2025). Box plots summarise visitor distributions at each camp. Most sites show low, tightly clustered counts, while Sweetwaters Tented Camp emerges as a clear hotspot with substantially higher occupancy and a marked outlier (≈208 visitors), illustrating how localised peaks are not captured by raster-based or conservancy-wide averages.
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Figure 7. Evolution of crew configurations across field campaigns. The initial setup (a) used four dedicated roles per UAS. The Multi-UAS setup (b) shared airspace and ground observers where fields of view overlapped. In the Swarm setup (c), synchronised missions allowed co-pilots to be shared. The Extended Field setup (d) merged the co-pilot and airspace-observer roles, with a 250 ft (75 m) AGL altitude limit to compensate for reduced airspace monitoring redundancy.
Figure 7. Evolution of crew configurations across field campaigns. The initial setup (a) used four dedicated roles per UAS. The Multi-UAS setup (b) shared airspace and ground observers where fields of view overlapped. In the Swarm setup (c), synchronised missions allowed co-pilots to be shared. The Extended Field setup (d) merged the co-pilot and airspace-observer roles, with a 250 ft (75 m) AGL altitude limit to compensate for reduced airspace monitoring redundancy.
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Figure 8. Efficiency gain per checklist through customisation, expressed as the reduction in checks relative to the baseline procedure set. Customised checklists were generated automatically by WildProcedures based on operation type and number of UAS. Most gains occur in the preparation stages before take-off, while later procedures remain unchanged due to their standardised structure.
Figure 8. Efficiency gain per checklist through customisation, expressed as the reduction in checks relative to the baseline procedure set. Customised checklists were generated automatically by WildProcedures based on operation type and number of UAS. Most gains occur in the preparation stages before take-off, while later procedures remain unchanged due to their standardised structure.
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Table 1. Summary of the calculation steps of the bottom-up population-density estimate.
Table 1. Summary of the calculation steps of the bottom-up population-density estimate.
ParameterEstimate
Projected annual visitors≈116,800
Daily visitors in January (seasonally adjusted)320 ± 10% → 352/day
Visitors per camp (10 sites)36 tourists/camp
Added staff per camp10 staff/camp
Total per camp46 people/camp
Area considered1 km2
Resulting population density46 people/km2
Table 2. Ground-risk exposure-reduction mitigations (M1): Measures to reduce the likelihood of uninvolved people being present within the operational footprint under SORA Annex B.
Table 2. Ground-risk exposure-reduction mitigations (M1): Measures to reduce the likelihood of uninvolved people being present within the operational footprint under SORA Annex B.
M1a
Sheltering
Low robustness. Most tourists remained inside safari vehicles or buildings when outdoors. Rangers operated mainly along roads and bush tracks, where vegetation, trees, and terrain features provided partial shielding.
M1b
Operational
restrictions
Medium robustness. Operations avoided overflying people and roads wherever possible. When road crossings were necessary, they were performed perpendicularly to minimise time above potential traffic. A 400 ft (120 m) horizontal buffer was applied around all campgrounds. Together, these restrictions reduced the proportion of the risk footprint where people may be present by more than 90%.
M1c
Observation
Low robustness. Remote crews conducted pre-flight and in-flight visual checks of the area and maintained continuous radio contact with the Ol Pejeta control room to identify gatherings or transient activity and adjust operations accordingly.
Table 3. Strategic air-risk mitigations: Measures to reduce the encounter rate with crewed aircraft.
Table 3. Strategic air-risk mitigations: Measures to reduce the encounter rate with crewed aircraft.
Altitude &
geography
Operations were capped at 400 ft (120 m) AGL west of the Ewaso River and 250 ft AGL east of it, the latter imposed by KAF due to proximity to Nanyuki Air Base. For BVLOS missions without observers, an internal ceiling of 250 ft (75 m)AGL was used to further reduce the risk of low-level encounters.
ChronologyDaytime flights were limited to a 2 km radius to ensure that visual observers could detect any approaching crewed aircraft with sufficient time to trigger contingency procedures. At night, when crewed aircraft are not permitted in this airspace, operations extended to 5 km.
Vertical
separation
A minimum 500 ft (150 m) separation was maintained between the operational ceiling and the published floor of crewed aviation.
Aerodrome
buffers
Exclusion zones of 9 km around Laikipia Airport and 5 km around Kamok Airstrip were removed from the operational volume (Figure 1).
External
coordination
For each flight period, the safety manager obtained KAF ATC approval for morning, afternoon, and evening slots to ensure coordinated use of the restricted airspace.
Table 4. Low-robustness TMPRs applied for ARC–b operations: The table summarises the layered detection approach, predefined contingency actions, command-and-control performance, execution times, and feedback latencies used to satisfy the Annex D low-robustness criteria.
Table 4. Low-robustness TMPRs applied for ARC–b operations: The table summarises the layered detection approach, predefined contingency actions, command-and-control performance, execution times, and feedback latencies used to satisfy the Annex D low-robustness criteria.
DetectDetection relied on three layers: (1) web-based traffic feeds (Flightradar24); (2) local 1090 MHz ADS-B reception via software-defined radio; (3) continuous aeronautical VHF monitoring. Each pilot was supported by an airspace observer equipped with binoculars, and extended-range BVLOS missions [2 km (day)/5 km (night)] included additional remote observers positioned at the far end of the flight path. These measures satisfy the Annex D requirement for low-robustness detection for ARC–b operations, although the true detection probability cannot be empirically verified due to the absence of ground-truth traffic data over the conservancy.
DecideWhen an intruder was detected, pilots executed predefined procedures: a rapid descent to below 100 ft (30 m), or if required, flight termination via the kill switch. Annex D specifies 60 ft (18 m) as the safe altitude; future campaigns will align with this value.
CommandCommand-and-control links used DJI OcuSync (O2/O3) or 2.4 GHz RC systems (WiFi, FrSky, Herelink). Measured latencies across all platforms, presented in Appendix B.10, remained
150 ms, well within the Annex D requirement of ≤5 s.
ExecuteThe slowest platform descended at 3 m/s, yielding a descent from 400 ft (120 m) to 60 ft (18 m) in 34 s, meeting the Annex D limit of ≤60 s (see Appendix B.10 for calculations).
FeedbackFeedback updates were required within 5 s and end-to-end latency below 10 s. Local ADS-B tracks refreshed every 1 s, and Flightradar24 updated at 2–3 s intervals [21].
Table 5. Summary of compliance with the Operational Safety Objectives (OSOs) applicable to a SAIL II operation. Detailed integrity and assurance justifications are provided in Appendix B.17.
Table 5. Summary of compliance with the Operational Safety Objectives (OSOs) applicable to a SAIL II operation. Detailed integrity and assurance justifications are provided in Appendix B.17.
OSOTitleStatusPrimary Limitation
#01Operator is competent and/or provenPartially metNo training and role records
#02UAS manufactured by competent and/or proven entityN/A (SAIL III+)
#03UAS maintained by competent/proven entityNot metNo formal maintenance system
#04UAS components essential to safe operations designed to ADSN/A (SAIL IV+)
#05UAS is designed considering system safety and reliabilityN/A (SAIL III+)
#06C3 link characteristics are appropriate for the operationMet
#07Conformity check of the UAS configurationPartially metNo conformity check procedure
#08Operational procedures defined, validated, adhered toPartially metNo ERP; limited assurance records
#09Remote crew trained and currentPartially metIncomplete training coverage
#13External services supporting operations are adequateMet
#16Multi-crew coordinationMet
#17Remote crew is fit to operateMet
#18Automatic protection of the flight envelope from human errorsN/A (SAIL III+)
#19Safe recovery from human errorN/A (SAIL III+)
#20Human Factors evaluation/HMI appropriate for missionPartially metNo formal HF evaluation
#23Environmental conditions defined, measurable, adhered toMet
#24UAS designed/qualified for adverse environmental conditionsN/A (SAIL III+)
Table 6. Crew-size optimisation across operation types. Summary of how crew refinements supported safe scaling as the number of UAS increased. Values indicate total personnel for each configuration and the reduction relative to the initial setup.
Table 6. Crew-size optimisation across operation types. Summary of how crew refinements supported safe scaling as the number of UAS increased. Values indicate total personnel for each configuration and the reduction relative to the initial setup.
Operation TypeUASCrew (Before)Crew (After)Reduction
Initial setup140%
Multi-UAS operations28625%
Swarm operations312650%
Extended field campaign4161225%
Table 7. Procedural adaptations across operation types during WildDrone 2025 field activities.
Table 7. Procedural adaptations across operation types during WildDrone 2025 field activities.
TypeKey Procedural AdaptationsUnderlying Rationale/Risk Context
Day/Night- Day: high-visibility vests, sun protection.
- Night: portable lights, warm clothing, strobe activation, and a mandatory daylight terrain survey.
Day missions focused on crew visibility; night missions required enhanced lighting and pre-survey of obstacles.
VLOS/BVLOS- VLOS: relied on line-of-sight communication.  
- BVLOS: added communication checks and, for longer ranges, VHF radios.
BVLOS requires additional communication and surveillance measures to maintain situational awareness.
BVLOS Sub-types- No remote observer: limited to 1 km from pilot.  
- With remote observer: up to 2 km with VHF and RLOS.
- Night BVLOS: up to 5 km with strobes and lighting.
Remote observer presence and time-of-day govern achievable range; longer distances require stronger mitigations.
Crew & Platform Variations- Single-UAS: baseline procedures.  
- Multiple-UAS: required pre-flight coordination, inter-pilot notification, and vertical separation.  
- Swarm: applied the same deconfliction principles with synchronised control under one operator.
Multi-UAS activities introduce shared airspace management needs. Vertical deconfliction prevents mid-air conflicts, and standardised templates support consistent application across platforms.
Common ElementsAirspace and weather checks, IMSAFE assessment, failsafe configuration, and post-flight logging were consistent.These steps ensured consistency and traceability across all operations.
Table 8. Efficiency gain (%) across operation types, shown as the reduction in checklist items relative to the non-customised baseline. Gains were highest for simpler configurations such as VLOS, with smaller improvements for multi-UAS and extended-range BVLOS operations.
Table 8. Efficiency gain (%) across operation types, shown as the reduction in checklist items relative to the non-customised baseline. Gains were highest for simpler configurations such as VLOS, with smaller improvements for multi-UAS and extended-range BVLOS operations.
VLOSBVLOS 1 kmBVLOS 1 kmBVLOS 1 kmBVLOS 2 kmNight BVLOSAverage
(single UAS)(single UAS)(multi-UAS)(swarm)(single UAS)5 km (single UAS)
22.6%20.2%16.7%19.0%15.5%13.1%17.9%
Table 9. Progressive refinement of operational procedures between January and March 2025.
Table 9. Progressive refinement of operational procedures between January and March 2025.
EvolutionKey Improvements and Outcomes
Procedures re-organisationChecklist structure was redesigned to separate one-time first-flight tasks from a shorter recurring checklist for subsequent flights, reducing repetition and cognitive workload while retaining essential safety steps.
Communication and role definitionEmergency and contingency procedures were made more explicit, with standard callouts, clear responsibilities, and contact numbers placed on the first page to support rapid response.
Containment standardisationCriteria for triggering Return-to-Home, land-on-site, or kill-switch actions were harmonised across operation types to improve crew familiarity and ensure consistent containment logic.
Threshold quantificationAmbiguous steps were replaced with measurable thresholds to increase repeatability, such as specifying landing-pad clearance distances and marking the site orientation.
Equipment requirementsPortable VHF/ADS-B units, originally carried universally, were later used only when required for higher-risk operations, with fixed equipment used otherwise.
Digital traceabilityDaily checklists were generated through WildProcedures with embedded time stamps and version identifiers, ensuring teams used consistent and traceable procedure sets.
Table 10. Summary of field operations conducted during and after the WildDrone Hackathon 2025.
Table 10. Summary of field operations conducted during and after the WildDrone Hackathon 2025.
Mission ObjectiveOperational Challenges & Lessons
#1Night tracking of lions (Panthera leo) to study movement and hunting behaviour.• Predator activity increases ground risk.
• Vehicle-based flying requires adaptations.
• Night conditions require audio logging.
• Fatigue management at night is essential.
• Fixed home point limits efficiency.
#2Evaluating a UAS swarm framework for coordinated, multi-perspective zebra monitoring [22,23,24].• Large teams reduce scalability.
• Short-range limits observation time.
• Vertical spacing limits fleet size.
• Procedural refinement boosts efficiency.
#3Assessing wildlife responses to controlled UAS approaches to study vigilance of Plains zebras.• Pre-flight setup minimises disturbance.
• Procedures training improves efficiency.
• Fixed home point limits flexibility.
#4Aerial photogrammetry of rhinos (Diceros bicornis, Ceratotherium simum) for individual recognition
and monitoring.
• Compact crew enhances flexibility.
• Low altitude disturbs wildlife.
• Range limits operational potential.
• Exclusion zones hinder monitoring.
• Co-development improves efficiency.• Crew training ensures readiness.
#53D reconstruction and semantic segmentation of savanna habitats for ecological modelling.• Dense vegetation increases collision risk.
• Bushland heightens wildlife risk.
• Field experience improves workflow.
#6Testing collaborative multi-UAS mapping methods for dynamic savanna environments [25].• Safety protocols limit crew scalability.
• Crew continuity improves familiarity.
#7Field-testing edge-AI systems (WildWing, WildLive) for autonomous wildlife tracking [26,27,28].• Custom platforms require adaptation.
• Standardisation enables fast onboarding.
#8Evaluating WildLive for real-time multi-species detection and tracking [27,28].• Higher altitude reduces tracking accuracy.
#9Assessing behavioural responses of large herbivores to UAS noise for ethical-flight guidance.• Large crews reduce scalability [29,30].
• Dual-UAS coordination increases workload.
• Safety procedures slow mission turnover.
• Range limits operational coverage.
• Crew training improves efficiency.
#10Evaluating geolocation and size-estimation accuracy using COTS UAS and monoplotting algorithms [31,32].• Crew optimisation improves efficiency.
• Routine operations risk complacency.
• Emergency training enhances readiness.
#11Testing a stereo-vision payload for non-invasive measurement of animal body condition.• Few pilots limit flexibility.
• Large platforms reduce agility.
• Short-range limits observation capacity.
• Procedural refinement improves efficiency.
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Maalouf, G.; Richardson, T.S.; Guerin, D.R.; Watson, M.; Lundquist, U.P.S.; Costelloe, B.R.; Pastucha, E.; Afridi, S.; Rolland, E.G.A.; Meier, K.; et al. SORA 2.5-Guided BVLOS UAS for Wildlife Conservation in Kenya: Reducing Friction Between Safety and Field Operations. Drones 2026, 10, 178. https://doi.org/10.3390/drones10030178

AMA Style

Maalouf G, Richardson TS, Guerin DR, Watson M, Lundquist UPS, Costelloe BR, Pastucha E, Afridi S, Rolland EGA, Meier K, et al. SORA 2.5-Guided BVLOS UAS for Wildlife Conservation in Kenya: Reducing Friction Between Safety and Field Operations. Drones. 2026; 10(3):178. https://doi.org/10.3390/drones10030178

Chicago/Turabian Style

Maalouf, Guy, Thomas Stuart Richardson, David Roy Guerin, Matthew Watson, Ulrik Pagh Schultz Lundquist, Blair R. Costelloe, Elzbieta Pastucha, Saadia Afridi, Edouard George Alain Rolland, Kilian Meier, and et al. 2026. "SORA 2.5-Guided BVLOS UAS for Wildlife Conservation in Kenya: Reducing Friction Between Safety and Field Operations" Drones 10, no. 3: 178. https://doi.org/10.3390/drones10030178

APA Style

Maalouf, G., Richardson, T. S., Guerin, D. R., Watson, M., Lundquist, U. P. S., Costelloe, B. R., Pastucha, E., Afridi, S., Rolland, E. G. A., Meier, K., Jepsen, J. H., Sterren, T. v. d., Laporte-Devylder, L., Saint-Jean, C. R., Catricheo, C. A. M., Shukla, V., Iannino, E., Kline, J., Ngoc, D. N., ... Jensen, K. (2026). SORA 2.5-Guided BVLOS UAS for Wildlife Conservation in Kenya: Reducing Friction Between Safety and Field Operations. Drones, 10(3), 178. https://doi.org/10.3390/drones10030178

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