An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft

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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)

Shaojie Zhang (Nanjing University of Aeronautics and Astronautics)

Xue Wu (Nanjing University of Aeronautics and Astronautics)

Erik-Jan van Kampen (TU Delft - Aerospace Engineering)

Qiping Chu (TU Delft - Aerospace Engineering)

Research Group

Control & Simulation

DOI related publication

https://doi.org/10.2514/6.2017-1253 Final published version

To reference this document use

https://resolver.tudelft.nl/uuid:e693923f-4907-445b-a6f9-5085383bdc0d

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Publication Year

2017

Language

English

Research Group

Control & Simulation

Article number

AIAA 2017-1253

ISBN (electronic)

978-1-62410-450-3

Event

AIAA Guidance, Navigation, and Control Conference, 2017 (2017-01-09 - 2017-01-13), Grapevine, United States

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Abstract

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