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

Journal article (2022)

Authors

J. Chang Xidian University, Aerospace Structures & Computational Mechanics - Aerospace Engineering
R. De Breuker Aerospace Structures & Computational Mechanics - Aerospace Engineering
Xuerui Wang Aerospace Structures & Computational Mechanics - Aerospace Engineering
Research Group
Aerospace Structures & Computational Mechanics (Aerospace Engineering) (TU Delft)
Copyright: © 2022 J. Chang, R. De Breuker, Xuerui Wang
DOI: https://doi.org/10.2514/1.G006690
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Published Date

2022

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Aerospace Structures & Computational Mechanics

Files

1.g006690.pdf
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- Embargo expired in 25-04-2023
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