Intelligent Control and Optimization of Electric Vertical Take-Off and Landing Unmanned Aerial Vehicles

A special issue of Drones (ISSN 2504-446X). This special issue belongs to the section "Drone Design and Development".

Deadline for manuscript submissions: 31 March 2026 | Viewed by 812

Special Issue Editors


E-Mail Website
Guest Editor
Department of Electrical and Computer Engineering, University of Alberta, Edmonton, AB T6G 1H9, Canada
Interests: EVTOL unmanned aerial vehicle; aerial transport; nonlinear control; adaptive control

E-Mail Website
Guest Editor
Department of Electrical and Computer Engineering, University of Alberta, Edmonton, AB T6G 1H9, Canada
Interests: EVTOL unmanned aerial vehicle; fault-tolerant control; nonlinear control; intelligent control

E-Mail Website
Guest Editor
Flight College, Shandong University of Aeronautics, Binzhou 256600, China
Interests: unmanned aerial vehicle; fault-tolerant control; nonlinear control; fault detection and diagnosis

Special Issue Information

Dear Colleagues,

Electric vertical take-off and landing (eVTOL) unmanned aerial vehicles (UAVs) are a category of aircraft equipped with multiple rotors, with or without tilting capabilities. They combine the functionalities of vertical take-off and landing with the ability to fly forward at high speeds. This unique capability makes them highly versatile, enabling them to address various applications that require velocity, agility, and long-range flight performance.

This Special Issue aims to present and promote the latest advancements in intelligent control strategies, optimization methods, and system design for eVTOL UAVs. However, the inherent challenges, including dynamic transition control, aerodynamic interference, power management, and safety redundancy, necessitate innovative approaches in intelligent control algorithms and optimization techniques.

The journal Drones focuses on the design, development, applications, and policy implications of eVTOL UAV systems, emphasizing advanced technologies, including aerodynamics, control systems, and real-world applications across civilian, industrial, and military sectors.

This Special Issue will collect original research articles and review papers that provide insights into the latest advancements, challenges, and opportunities in enhancing the performance, automation, and reliability of eVTOL UAVs through intelligent control strategies and optimization techniques. It aims to bridge the gap between theoretical research and practical applications, focusing on innovations which address challenges in flight dynamics, energy efficiency, real-time decision making, and mission planning for eVTOL UAVs.

This Special Issue will welcome manuscripts that link the following themes:

  • Intelligent control strategies for flight control;
  • Optimization techniques in autonomous navigation and motion control;
  • Fault detection and diagnosis for eVTOL

We look forward to receiving your contributions.

Dr. Zongyang Lv
Prof. Dr. Qing Zhao
Dr. Hao Wei
Guest Editors

Manuscript Submission Information

Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.

Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Drones is an international peer-reviewed open access monthly journal published by MDPI.

Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2600 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.

Keywords

  • eVTOL
  • UAV
  • optimal control
  • intelligent control
  • nonlinear control
  • fault-tolerant control

Benefits of Publishing in a Special Issue

  • Ease of navigation: Grouping papers by topic helps scholars navigate broad scope journals more efficiently.
  • Greater discoverability: Special Issues support the reach and impact of scientific research. Articles in Special Issues are more discoverable and cited more frequently.
  • Expansion of research network: Special Issues facilitate connections among authors, fostering scientific collaborations.
  • External promotion: Articles in Special Issues are often promoted through the journal's social media, increasing their visibility.
  • Reprint: MDPI Books provides the opportunity to republish successful Special Issues in book format, both online and in print.

Further information on MDPI's Special Issue policies can be found here.

Published Papers (1 paper)

Order results
Result details
Select all
Export citation of selected articles as:

Research

43 pages, 4153 KB  
Article
Initial Weight Modeling and Parameter Optimization for Collectible Rotor Hybrid Aircraft in Conceptual Design Stage
by Menglin Yang, Zhiqiang Wan, De Yan, Jingwei Chen and Ruihan Dong
Drones 2025, 9(10), 690; https://doi.org/10.3390/drones9100690 - 7 Oct 2025
Viewed by 311
Abstract
A collectible rotor hybrid aircraft (CRHA) represents a novel type of vertical takeoff and landing (VTOL) unmanned aircraft configuration, combining the typical rotor and transmission systems of helicopters with the wing and propulsion systems of fixed-wing aircraft. Its weight estimation and parameter design [...] Read more.
A collectible rotor hybrid aircraft (CRHA) represents a novel type of vertical takeoff and landing (VTOL) unmanned aircraft configuration, combining the typical rotor and transmission systems of helicopters with the wing and propulsion systems of fixed-wing aircraft. Its weight estimation and parameter design during the conceptual design stage cannot directly use existing rotorcraft or fixed-wing methods. This paper presents a rapid key design parameter sizing and maximum takeoff weight (MTOW) estimation approach tailored to CRHA, explicitly scoped to the 5–8-metric-ton (t) MTOW class. Component weight models are first formulated as explicit functions of key design parameters—including rotor disk loading, power loading, and wing loading. Segment-specific fuel weight fractions for VTOL and transition flight are then updated from power calculations, yielding a complete mission fuel model for this weight class. A hybrid optimization framework that minimizes MTOW is constructed by treating the key design parameters as design variables and combining a genetic algorithm (GA) with sequential quadratic programming (SQP). The empty-weight model, fuel-weight model, and optimization framework are validated against compound-helicopter, tilt-rotor, and twin-turboprop benchmarks, and parameter sensitivities are evaluated locally and globally. Results show prediction errors of roughly 10% for empty weight, fuel weight, and MTOW. Sensitivity analysis indicates that at the baseline design point, wing loading exerts the greatest influence on MTOW, followed by power loading and disk loading. Full article
Show Figures

Figure 1

Back to TopTop