Multi-objective integrated robust H∞ control for attitude tracking of a flexible spacecraft

Wu, S., Chu, W., Ma, X., Radice, G. and Wu, Z. (2018) Multi-objective integrated robust H∞ control for attitude tracking of a flexible spacecraft. Acta Astronautica, 151, pp. 80-87. (doi: 10.1016/j.actaastro.2018.05.062)

Abstract

This paper investigates the multi-objective attitude tracking problem of a flexible spacecraft in the presence of disturbances, parameter uncertainties and imprecise collocation of sensors and actuators. An integrated robust H∞ controller, including an output feedback component and a feedforward component, is proposed, and its gains are calculated by solving Linear Matrix Inequalities. The output feedback component stabilizes the integrated control system while the feedforward component can drive the attitude motion to track the desired angles. The system robustness against disturbances, parameter uncertainties and imprecise collocation is addressed by the H∞ approach and convex optimization. Numerical simulations are finally provided to assess the performance of the proposed controller.

• Item Type: Articles
• Additional Information: This work is supported by the National Natural Science Foundation of China (11502040 & 11502017), and the Fundamental Research Funds for the Central Universities (DUT18GF304).
• Status: Published
• Refereed: Yes
• Glasgow Author(s) Enlighten ID: Radice, Dr Gianmarco
• Authors: Wu, S., Chu, W., Ma, X., Radice, G., and Wu, Z.
• College/School: College of Science and Engineering > School of Engineering
• Journal Name: Acta Astronautica
• Publisher: Elsevier
• ISSN: 0094-5765
• Published Online: 01 June 2018
• Copyright Holders: Copyright © 2018 IAA
• First Published: First published in Acta Astronautica 151: 80-87
• Publisher Policy: Reproduced in accordance with the publisher copyright policy