Active Fault-Tolerant Incremental Sliding-Mode Flight Control Against Control Reversal-Reference-Cited by-同舟云学术

Active Fault-Tolerant Incremental Sliding-Mode Flight Control Against Control Reversal

Published:2022-12 Issue:12 Volume:45 Page:2411-2420
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Chang Jing¹,De Breuker Roeland²^ORCID,Wang Xuerui²^ORCID

Affiliation:

1. Xidian University, 710126 Xi’an, People’s Republic of China

2. Delft University of Technology, 2629 HS Delft, The Netherlands

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G006690

Reference29 articles.

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3. DayR. E., Coupling Dynamics in Aircraft: a Historical Perspective, Vol. 532, Office of Management, Scientific and Technical Information Program, NASA, Washington, D.C., 1997, pp. 2–4.

4. Evaluation of an L1 Adaptive Flight Control Law on Calspan’s Variable-Stability Learjet

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