Sliding Mode based Path Planning and Control of Impaired Aircraft
Abstract
In this study, the problem of integrated path planning and control of an impaired aircraft is formulated and solved by using a second order sliding mode control (SOSM) and a high order sliding mode (HOSM) differentiator. As an example problem, the case of an impaired aircraft with a frozen elevator is considered. The thrust alone is used as the controller to land the aircraft safely. Representative simulations are presented to demonstrate the performance of proposed controller.
Recommended Citation
M. Deniz et al., "Sliding Mode based Path Planning and Control of Impaired Aircraft," Proceedings of the AIAA Scitech 2019 Forum (2019, San Diego, CA), American Institute of Aeronautics and Astronautics (AIAA), Jan 2019.
The definitive version is available at https://doi.org/10.2514/6.2019-0931
Meeting Name
AIAA Scitech Forum, 2019 (2019: Jan. 7-11, San Diego, CA)
Department(s)
Mechanical and Aerospace Engineering
Keywords and Phrases
Aircraft; Aircraft control; Aviation; Controllers; Motion planning, Differentiators; High order sliding mode; Path planning and control; Second-order sliding-mode control; Sliding modes, Sliding mode control
International Standard Book Number (ISBN)
978-162410578-4
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2019 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
01 Jan 2019
Comments
This study was supported in part by the NASA grants NNX15AM51A and NNX15AN04A.