Design Principle of Non-Switching Integral Sliding Mode Controller and Applications to Aerospace Vehicles

Kawai, Y., Uchiyama, K. and McInnes, C. R. (2018) Design Principle of Non-Switching Integral Sliding Mode Controller and Applications to Aerospace Vehicles. In: 2018 AIAA Guidance, Navigation, and Control Conference, Kissimmee, FL, USA, 08-12 Jan 2018, ISBN 9781624105265 (doi: 10.2514/6.2018-0857)

Abstract

This paper proposes a new type of sliding mode controller termed non-switching integral sliding mode controller. It shows a certain robustness of the control system against matched uncertainty with non-switching input. Furthermore, it allows the control system to be analyzed from the aspects of the system norms, small gain theorem, and structured singular value. The validities of the proposed controller are shown by performing the numerical simulations for three different applications: a spacecraft in a displaced non-Keplerian orbit, a soft-landing problem, and a quadcopter carrying a manipulator. The potential of the proposed sliding mode control methodology is demonstrated numerically for versatility in the applications.

• Item Type: Conference Proceedings
• Status: Published
• Refereed: Yes
• Glasgow Author(s) Enlighten ID: McInnes, Professor Colin
• Authors: Kawai, Y., Uchiyama, K., and McInnes, C. R.
• College/School: College of Science and Engineering > School of Engineering > Systems Power and Energy
• ISBN: 9781624105265
• Copyright Holders: Copyright © 2018 American Institute of Aeronautics and Astronautics, Inc.
• First Published: First published in 2018 AIAA Guidance, Navigation, and Control Conference
• Publisher Policy: Reproduced in accordance with the publisher copyright policy