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Aerospace, Volume 13, Issue 3

2026 March - 92 articles

Cover Story: The ever-growing number of debris comprising rocket bodies and defunct satellites in orbit around the Earth has shifted the interest of space agencies towards the development of reliable GNC systems for non-cooperative rendezvous missions. Such efforts demand on-board software solutions to enable the servicer spacecraft to autonomously approach the client in a safe manner. Within this context, the current study details the design and validation of a rule-based guidance architecture that leverages existing closed-form impulsive maneuvering schemes and extends their formulation to arbitrarily elliptic orbits. The results show that the proposed design can feasibly be used as a general baseline across different mission scenarios. View this paper
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Articles (92)

  • Article
  • Open Access
747 Views
31 Pages

Rotor-flexible casing rubbing can induce strong nonlinear dynamics in rotor systems. This study investigates the harmonic frequency characteristics of a rubbing rotor system with a flexible casing constraint. A nonlinear rub-impact model combined wit...

(This article belongs to the Special Issue Aircraft Structural Dynamics)
  • Review
  • Open Access
3 Citations
24,986 Views
84 Pages

A review of morphing actuation systems in relation to rotary-wing aerial platforms is presented. The research highlights an inadequate maturation of rotary actuation systems, characterised by a scarcity of (1) comprehensive full-scale experimental re...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
4 Citations
1,333 Views
35 Pages

EO-MADDPG: An Improved Reinforcement Learning Approach for Multi-UAV Pursuit–Evasion Games

  • Xiao Wang,
  • Mengyu Wang,
  • Xueqian Bai,
  • Zhe Ma and ,
  • Kewu Sun and
  • Jiake Li
  • + 1 author+ 0 author

To advance research in multi-agent reinforcement learning (MARL) for pursuit–evasion scenarios, this paper introduces a novel algorithm called Expert Knowledge and Opponent Modeling Multi-UAV Deep Deterministic Policy Gradient (EO-MADDPG). EO-M...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1,154 Views
25 Pages

The remain well clear (RWC) function of a detect-and-avoid (DAA) system provides guidance to a remote pilot (RP) of a remotely piloted aircraft to prevent a conflict from developing into a collision hazard. The ACAS Xu standard is a decision support...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
2 Citations
1,652 Views
15 Pages

Enabling Scalable and Efficient Low-Altitude Airspace Utilization for Dense Urban Operations

  • Yamin Zhang,
  • Rong Xu,
  • Bin Hu,
  • Kaiyu Nie and ,
  • Hang Zhao,
  • Bo Chen and
  • Qinglei Kong
  • + 2 authors+ 0 author

The rapid growth of low-altitude air traffic demands airspace evaluation frameworks that are scalable, flexible, and efficient. However, existing airspace partitioning strategies, primarily designed for sparse, long-distance civil aviation, are ill-s...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
1,184 Views
20 Pages

The design day flight schedule (DDFS) plays a pivotal role in airport simulation and infrastructure planning. Despite its importance, previous studies and global guidelines offer only broad recommendations for DDFS preparation, lacking detailed metho...

(This article belongs to the Special Issue Next-Generation Airport Operations and Management)
  • Article
  • Open Access
1 Citations
644 Views
22 Pages

New, highly integrated, disruptive aircraft concepts are being devised to reduce aviation’s environmental footprint, but their performance is oftentimes challenging for the aircraft designer to assess. Furthermore, these novel aircraft often in...

(This article belongs to the Special Issue 15th EASN International Conference on Innovation in Aviation & Space Towards Sustainability Today and Tomorrow)
  • Article
  • Open Access
3 Citations
2,065 Views
27 Pages

An Ultra-High-Aspect-Ratio Telescopic Continuum Robot Design for Aero-Engine Borescope Inspection

  • Da Hong,
  • Yuancan Huang,
  • Nianfeng Shao,
  • Yiming Wang and
  • Weiheng Zhong

Conventional borescopes are limited by inadequate mechanical flexibility, poor environmental adaptability and reachability, and heavy reliance on operator expertise during aero-engine inspections, making it difficult to meet the demands for efficient...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
713 Views
28 Pages

As a critical actuator in aero-engine control systems, the health condition of the Fuel Metering Unit (FMU) directly influences flight safety and maintenance efficiency, making the precise prediction of its degradation process a core task in the engi...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
810 Views
23 Pages

In this study, a novel hybrid optimization approach is proposed to minimize the fuel consumption of commercial aircraft by taking flight-related and meteorological constraints into account during the cruise phase. The new method, the Decision Tree&nd...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1,087 Views
16 Pages

Shape Optimization of Aircraft Outflow Valve for Maximum Thrust Recovery

  • Tasos Karageorgiou,
  • Pela Katsapoxaki,
  • Michael Moeller and
  • El Hassan Ridouane

The present study demonstrates a step-by-step method for optimizing the outflow valve geometry and maximizing thrust generation. In this system, the skin-mounted OutFlow Valve (OFV) acts as a convergent–divergent nozzle and, as such, the De Lav...

(This article belongs to the Special Issue 15th EASN International Conference on Innovation in Aviation & Space Towards Sustainability Today and Tomorrow)
  • Review
  • Open Access
2 Citations
2,533 Views
28 Pages

Light-Curve Classification of Resident Space Objects for Space Situational Awareness: A Scoping Review

  • Minyoung Hwang,
  • Vithurshan Suthakar,
  • Randa Qashoa,
  • Regina S. K. Lee and
  • Gunho Sohn

The proliferation of Resident Space Objects (RSOs), including satellites, rocket bodies, and debris, poses escalating challenges for Space Situational Awareness (SSA). Optical light curves capture temporal brightness variations influenced by factors...

(This article belongs to the Special Issue Advances in Space Surveillance and Tracking)
  • Article
  • Open Access
2 Citations
1,483 Views
25 Pages

The increasing adoption of high-aspect-ratio wings to improve aerodynamic efficiency introduces significant structural flexibility, necessitating the integration of aeroelastic considerations into the earliest design stages. While critical, existing...

(This article belongs to the Special Issue 15th EASN International Conference on Innovation in Aviation & Space Towards Sustainability Today and Tomorrow)
  • Article
  • Open Access
1 Citations
1,238 Views
19 Pages

In low-Earth-orbit (LEO) satellite networks, the need for intelligent parameter-adjustment strategies has become increasingly critical due to the presence of highly dynamic channel conditions, limited spectrum resources, and complex interference envi...

(This article belongs to the Special Issue Advanced Spacecraft/Satellite Technologies (2nd Edition))
  • Article
  • Open Access
1,308 Views
27 Pages

A Simulation and TOPSIS Approach to the Satellite Constellation Design Problem

  • Mikkel Søby Kramer,
  • Frederik Christensen,
  • Veronica Hjort,
  • Peter Nielsen and
  • Alex Elkjær Vasegaard

The design of satellite constellations is a complex optimization problem interdependent with other decision problems and multiple competing, user-specific criteria. Consequently, it is very difficult to make a final decision on the constellation desi...

(This article belongs to the Special Issue Decision-Making Strategies for Aerospace Mission Design and Planning)
  • Article
  • Open Access
1,080 Views
25 Pages

Reentry Trajectory Optimization of Hypersonic Vehicle Based on Multi-Strategy Improved WOA Optimized Attention-LSTM Network

  • Encheng Dai,
  • Guangbin Cai,
  • Yonghua Fan,
  • Hui Xu and ,
  • Hao Wei and
  • Xin Li
  • + 1 author+ 0 author

Trajectory optimization of hypersonic vehicles face challenges from complex aerodynamic environments and multiple constraints, where traditional offline optimization methods struggle to meet real-time requirements. This study proposes a novel online...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
628 Views
24 Pages

Space-based multi-target passive tracking is critical for space situational awareness, but faces severe challenges due to the limited field-of-view (FoV) and directional ambiguity of onboard sensors. These constraints often lead to target loss, poor...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1,013 Views
23 Pages

This paper proposes a data-driven model for predicting rotor fluid-structure interaction (FSI) load with efficient aeroelastic analysis. Unsteady flow-field snapshots obtained from computational fluid dynamics (CFD) simulations are first processed us...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1,330 Views
19 Pages

This work presents a space-oriented extension of an existing research program focused on developing innovative approaches and design solutions for rotorcraft. The study builds upon recent research conducted at the Military University of Technology, w...

(This article belongs to the Special Issue 15th EASN International Conference on Innovation in Aviation & Space Towards Sustainability Today and Tomorrow)
  • Article
  • Open Access
916 Views
27 Pages

Orbit-Prior-Guided Target-Centered Stacking for Space Surveillance and Tracking Under Dynamic-Platform Optical Observations

  • Lanze Qu,
  • Junchi Liu,
  • Hongwen Li,
  • Zhiyong Wu and ,
  • Jianli Wang and
  • Kainan Yao
  • + 1 author+ 0 author

In visible-light optical observations for Space Surveillance and Tracking (SST) from ground-based dynamic platforms, attitude disturbances and field-of-view discontinuities frequently undermine interframe geometric consistency, leading to energy diff...

(This article belongs to the Special Issue Advances in Space Surveillance and Tracking)
  • Article
  • Open Access
3 Citations
2,345 Views
22 Pages

Thermo-Mechanical Design of the C/C-SiC-Based Thermal Protection Structure for the Forebody of the Hypersonic Sounding Rocket STORT

  • Giuseppe Daniele Di Martino,
  • Thomas Reimer,
  • Luis Baier,
  • Lucas Dauth and ,
  • Dorian Hargarten and
  • Ali Gülhan
  • + 1 author+ 0 author

Re-entry flights of reusable first or upper stages typically foresee phases in the hypersonic flight regime, characterized by severe aero-thermal loads which could become critical for the most exposed components, like the vehicle forebody or the fin...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
1,157 Views
20 Pages

Low Earth orbit (LEO) satellite networks require real-time routing to cope with dynamic topology variations caused by continuous orbital motion. As an alternative to conventional routing approaches, deep reinforcement learning (DRL) has recently gain...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1 Citations
1,197 Views
29 Pages

Dynamic Trajectory Planning for Autonomous Parafoil Homing Under Wind Disturbances

  • Luqi Yan,
  • Yanguo Song,
  • Huanjin Wang,
  • Zhiwei Shi and
  • Yilei Song

The parafoil is highly susceptible to deviations from its reference trajectory under wind disturbances. Given its constrained longitudinal control authority, it has limited capability to correct these deviations and regain the intended glide path. To...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
781 Views
27 Pages

Owing to its large flexible envelope, an airship is highly sensitive to environmental disturbances, such as wind gusts. Fluid–structure interaction induces structural deformation, which modifies the aerodynamic force distribution and introduces...

(This article belongs to the Special Issue Design, Characterization and Operations of Lighter-than-Air Flying Vehicles)
  • Article
  • Open Access
790 Views
19 Pages

Experimental Quantization of Droplet Spatial Distribution in Icing Wind Tunnel with HACPI

  • Letian Zhang,
  • Boyi Wang,
  • Yingchun Wu,
  • Si Li and ,
  • Zhiqiang Zhang,
  • Xiangdong Guo,
  • Xuecheng Wu,
  • Quanzhong Xia and
  • Zhen Liu
  • + 4 authors+ 0 author

The cloud spatial uniformity in the test section is crucial for icing wind tunnels in aircraft icing research and airworthiness certification. To achieve uniform supercooled large droplet (SLD) icing conditions, both the spatial variation in droplet...

(This article belongs to the Special Issue Deicing and Anti-Icing of Aircraft (Volume IV))
  • Article
  • Open Access
734 Views
19 Pages

With the rapid development of the aviation industry, engines operate under extreme conditions of high temperature, high pressure, and high vibration, making them prone to surface damage such as ablation. Ablation not only affects the structural integ...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
849 Views
21 Pages

To improve the punctuality of flight schedules, causal inference methods are introduced to model the potential causal structure and intervention effects among ground support operations of flights. The effectiveness of these methods in improving fligh...

(This article belongs to the Special Issue Emerging Trends in Air Traffic Flow and Airport Operations Control)
  • Article
  • Open Access
1 Citations
935 Views
31 Pages

Civil aviation VHF communication is safety-critical, yet operational links are routinely disturbed by atmospheric effects, aging hardware, and electromagnetic interference. The resulting anomalies are typically weak, intermittent, and extremely rare,...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
756 Views
23 Pages

Low Earth Orbit (LEO) satellite signals of opportunity (SOP) provide a viable positioning alternative in GNSS (Global Navigation Satellite System)-denied environments, yet their accuracy is fundamentally constrained by the low-quality orbital data ty...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1 Citations
652 Views
26 Pages

Tiltable quadrotors have the ability of independent control of position and attitude, which can be more flexible in complex task scenarios. However, the inherent unmodeled dynamics, model uncertainties, and external disturbances pose significant chal...

(This article belongs to the Section Aeronautics)
  • Editorial
  • Open Access
1,089 Views
4 Pages

Urban low-altitude traffic systems are an emerging and transformative urban transportation system, promising to revolutionize how people and goods move within and between cities [...]

(This article belongs to the Special Issue Research and Applications of Low-Altitude Urban Traffic System)
  • Article
  • Open Access
2 Citations
676 Views
21 Pages

Study on the Influence of Soil Parameters on the Cushioning Performance of Landing Airbags

  • Yichen Wang,
  • Xuan Zhou,
  • Jingang Liu,
  • Xiaolun Li and ,
  • Jiang Wang and
  • Pei Zhang
  • + 1 author+ 0 author

To investigate the influence of soil parameters on the cushioning performance of landing airbags, a landing airbag cushioning dynamics model considering soil characteristics was established based on the control volume method and a crushable foam mode...

(This article belongs to the Special Issue Advances in Landing Systems Engineering)
  • Editorial
  • Open Access
548 Views
3 Pages

Special Issue: Numerical Simulations in Electric Propulsion

  • Nabil Souhair,
  • Fabrizio Ponti,
  • Mirko Magarotto and
  • Vittorio Giannetti

Electric propulsion (EP) has become a key enabling technology for a wide range of space missions, including orbit raising and station keeping, deep-space exploration, and emerging applications such as very-low Earth orbit (VLEO) platforms and small s...

(This article belongs to the Special Issue Numerical Simulations in Electric Propulsion)
  • Article
  • Open Access
1,100 Views
16 Pages

Reynolds Number Effect of a Supercritical Wing Based on Cryogenic and High Reynolds Number Pressure Test

  • Baobin Hou,
  • Yanru Chen,
  • Jinyan Cai,
  • Xin Peng and ,
  • Xin Xu and
  • Dawei Liu
  • + 1 author+ 0 author

Supercritical wings are widely used in large aircraft due to their excellent transonic performance, but their aerodynamic characteristics are highly sensitive to Reynolds number. To systematically study the influence of Reynolds number on the aerodyn...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
1,190 Views
36 Pages

Optimised SBAS Ground Segment for Colombia Using Traffic and Ionospheric Risk Models

  • Jaime Enrique Orduy,
  • Sebastian Valencia,
  • Felipe Rodriguez,
  • Cristian Lozano and ,
  • Juan Mosquera and
  • Christian Rincon
  • + 1 author+ 0 author

This paper presents the design, optimization, and performance evaluation of a Satellite-Based Augmentation System (SBAS) ground segment tailored to Colombia’s air navigation infrastructure, with emphasis on ionospheric anomalies in equatorial l...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
929 Views
25 Pages

Transient Modeling and Analysis of Short-Circuit Faults in the DC Power System for Hybrid Electric Aircraft

  • Bin Liu,
  • Shuguang Wei,
  • Jiaqi Li,
  • Kewei Chen and ,
  • Feifan Xu and
  • Hengliang Zhang
  • + 1 author+ 0 author

Transient modeling of short-circuit faults in the DC power system of hybrid electric aircraft (HEA) serves as a fundamental basis for effective fault identification, localization, and isolation. Before faults are detected and protective measures are...

  • Article
  • Open Access
3 Citations
2,442 Views
29 Pages

This study investigates hybridization of a solid oxide fuel cell with a gas turbine (SOFC–GT) for application in an ATR 72 regional aircraft. Several challenges hinder its viability, including the low gravimetric power density of SOFC stacks an...

(This article belongs to the Special Issue 15th EASN International Conference on Innovation in Aviation & Space Towards Sustainability Today and Tomorrow)
  • Article
  • Open Access
466 Views
21 Pages

Sliding Mode Control (SMC) is a widely used controlling method in the field of current attitude control of launch vehicles. The effectiveness of reaching the Sliding Surface could influence the effect of the attitude control. Aiming to derive better...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1 Citations
898 Views
15 Pages

Aircraft icing prediction is crucial for aerodynamic design and airworthiness assessment. Traditional physics-based models struggle with complex multi-physical processes, while existing AI methods (function-based characterization or direct image lear...

(This article belongs to the Special Issue Aerospace Vehicle Optimization: Design Innovations, Thermal Management, and Practical Applications)
  • Review
  • Open Access
2 Citations
3,231 Views
31 Pages

Detonation Waves on Enhancing Aerospace Propulsion Systems Performances: A Review

  • Bogdan-Cătălin Năvligu,
  • Grigore Cican,
  • Răzvan Edmond Nicoară and
  • Theodor-Mihnea Sîrbu

Detonation-based combustion has re-emerged as a promising pathway for enhancing the efficiency and compactness of future aerospace propulsion systems, motivated by the intrinsic pressure-gain characteristics of detonative heat release. This review pr...

(This article belongs to the Special Issue Space Propulsion: Advances and Challenges (4th Edition))
  • Article
  • Open Access
3 Citations
1,253 Views
21 Pages

Complex Illumination-Aware 3D Gaussian Reconstruction for Uncooperative Space Objects

  • Ziang Qu,
  • Zhang Zhang,
  • Ruiqi Xun,
  • Junlan Zhou and
  • Liang Chang

High-precision 3D reconstruction of non-cooperative space targets is a critical technology for on-orbit servicing (OOS) and situational awareness, driven by the growing number of OOS missions. However, traditional visual algorithms struggle to acquir...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1,157 Views
29 Pages

The safety-critical nature of aircraft landing gear has led to interest in Structural Health Monitoring (SHM) and Remaining Useful Life (RUL) methodologies for the fatigue substantiation of landing gear assemblies. Due to the engineering effort that...

(This article belongs to the Special Issue Advances in Landing Systems Engineering)
  • Article
  • Open Access
754 Views
22 Pages

Short-wave infrared star sensors have become a key technology for all-time attitude determination within the atmosphere, in which the star identification algorithm plays a fundamental role. However, due to the limited number of detectable stars in in...

(This article belongs to the Special Issue Recent Advances in Vehicle Navigation and Positioning)
  • Article
  • Open Access
1 Citations
1,310 Views
23 Pages

High-performance geared turbofan engines generate significant heat within the planetary power gearbox. This study presents the thermal design of an integrated fan guide vane heat exchanger aimed at recovering gearbox heat losses with minimal pressure...

(This article belongs to the Special Issue 15th EASN International Conference on Innovation in Aviation & Space Towards Sustainability Today and Tomorrow)
  • Feature Paper
  • Article
  • Open Access
1 Citations
734 Views
35 Pages

High−Altitude wind is a critical factor affecting the recovery safety of reusable rockets, significantly altering aerodynamic loads, flight attitudes, and trajectories—especially during the aerodynamic deceleration phase (engine shutdown)...

  • Article
  • Open Access
719 Views
19 Pages

Considering the challenges currently faced in the civil air traffic management (ATM) domain, this study investigates an aircraft safety situation awareness method based on ADS-B surveillance data. First, a sector safety situation assessment framework...

  • Article
  • Open Access
1 Citations
704 Views
18 Pages

Whether the inlet can start successfully is a prerequisite for the propulsion system to provide normal power to an aircraft. To address the starting difficulty of a high-contraction-ratio TBCC inlet lacking self-starting capability, this study propos...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
1,197 Views
21 Pages

Sustainable aviation requires electrical power systems that can deliver both high energy and high power. Hybrid fuel cell–battery architectures offer a promising solution to meet these demands, and their overall performance can be significantly...

(This article belongs to the Special Issue 15th EASN International Conference on Innovation in Aviation & Space Towards Sustainability Today and Tomorrow)
  • Article
  • Open Access
1,003 Views
27 Pages

Constraint-Aware Payload Layer Fusion Control for Dual-Quadrotor Cooperative Slung-Load Transportation

  • Xi Wang,
  • Pengliang Zhao,
  • Xing Wang,
  • Weihua Tan and ,
  • Hongqiang Zhang,
  • Jiwen Zeng and
  • Shasha Tang
  • + 2 authors+ 0 author

Low altitude logistics and aerial transport increasingly rely on multirotor unmanned aerial vehicles (UAVs) carrying slung payloads, where cable flexibility and load swing can degrade safety and delivery accuracy. This paper studies payload trajector...

(This article belongs to the Section Aeronautics)
  • Review
  • Open Access
4 Citations
4,882 Views
39 Pages

A Comprehensive Literature Review of Cybersecurity in Satellite Networks

  • Buhong Wang,
  • Jin Xiao,
  • Ruochen Dong,
  • Chengkai Piao and ,
  • Yongjian Guan,
  • Bofu Zhao,
  • Yong Yang,
  • Zhengyang Zhao,
  • Siqi Li and
  • Xiaofan Lyu
  • + 5 authors+ 0 author

Satellite networks are essential to global connectivity yet face severe multidimensional cybersecurity threats. This systematic review conducts a holistic analysis of threats across the physical, network, and user layers. We propose the Sat-ATT&C...

(This article belongs to the Section Astronautics & Space Science)

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Aerospace - ISSN 2226-4310