An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft
Conference Paper
(2017)
Author(s)
Weifang Shuang (Nanjing University of Aeronautics and Astronautics)
S. Zhang (Nanjing University of Aeronautics and Astronautics)
Xue Wu (Nanjing University of Aeronautics and Astronautics)
EJ Kampen (TU Delft - Control & Simulation)
Q. P. Chu (TU Delft - Control & Simulation)
Research Group
Control & Simulation
Copyright
© 2017 Weifang Shuang, S. Zhang, Xue Wu, E. van Kampen, Q. P. Chu
DOI related publication
https://doi.org/10.2514/6.2017-1253
To reference this document use:
https://resolver.tudelft.nl/uuid:e693923f-4907-445b-a6f9-5085383bdc0d
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Publication Year
2017
Language
English
Copyright
© 2017 Weifang Shuang, S. Zhang, Xue Wu, E. van Kampen, Q. P. Chu
Research Group
Control & Simulation
ISBN (electronic)
978-1-62410-450-3
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.
Abstract
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