Challenges and Innovations in Aircraft Flight Control

A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".

Deadline for manuscript submissions: 31 August 2024 | Viewed by 154

Special Issue Editors


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Guest Editor
School of Engineering, University of Leicester, Leicester LE1 7RH, UK
Interests: guidance, navigation, and control for uncrewed aerial vehicles (UAVs); crewed aircraft and electric vertical takeoff and landing vehicles

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Guest Editor
School of Aerospace, Transport and Manufacturing, Cranfield University, Cranfield MK43 0AL, UK
Interests: guidance, navigation, and control of aerial systems; robust and adaptive control theory; unmanned traffic management

Special Issue Information

Dear Colleagues,

Recent years have seen a rise in the aircraft performance, safety, and autonomy requirements for both crewed and uncrewed aircraft. This is creating new flight control challenges for different classes of aircraft. Civilian airliners are evolving towards increasing their levels of automation, but this is creating flight control safety challenges. Uncrewed aerial vehicles (UAVs) have also evolved with an unprecedented variety in their designs. Aircraft control systems are also increasingly required to save energy and reduce emissions, particularly in the case of electric aircraft, including urban air mobility.

In this Special Issue, particular prominence will be given to the development of estimation and control methods and algorithms for:

- Fault tolerant aircraft control systems under sensor and actuator faults;

- Optimal aircraft control allocation using multiple actuators;

- Flight envelope protection for enhanced flight safety;

- Optimal aircraft control problems of practical significance, including energy optimality, optimal tradeoffs, time optimality, and optimal coverage path planning;

- Adaptive flight control to handle aircraft parameter variations;

- Aircraft state, fault, disturbance, and model uncertainty estimation using advances in observers, Kalman filters, and other estimation methods;

- Advances in aircraft robust control;

- Hybrid (combined continuous and discrete time) control approaches for flight profiles with multiple flight modes;

- Artificial intelligence in flight control;

- Advances in the control of hybrid (cruise and VTOL) aircraft configurations;

- Combining open-loop and closed-loop aircraft control systems;

- Advances in autonomous and full authority flight control systems.

Review, theoretical, simulation-based, and practical-type papers are all within the scope of this Special Issue. All aircraft types are also within the scope of this Special Issue.

Dr. Nadjim Horri
Dr. Toufik Souanef
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. Aerospace 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 2400 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

  • UAV
  • electric aircraft
  • fault
  • disturbance
  • optimal
  • robust control
  • adaptive
  • hybrid control

Published Papers

This special issue is now open for submission.
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