Title

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.

Meeting Name

AIAA Scitech Forum, 2019 (2019: Jan. 7-11, San Diego, CA)

Department(s)

Mechanical and Aerospace Engineering

Comments

This study was supported in part by the NASA grants NNX15AM51A and NNX15AN04A.

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.

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