Prediction-based sampled-data H∞ controller design for attitude stabilisation of a rigid spacecraft with disturbances. Issue 11 (18th August 2017)

• Record Type: Journal Article
• Authors: Zhu, Baolong; Zhang, Zhiping; Zhou, Ding; Ma, Jie; Li, Shunli
• Is Part Of: International journal of systems science. Volume 48:Issue 11(2017)
• Page Start: 2356
• Page End: 2367
• Publication Date: 2017-08-18
• Subjects: Rigid spacecraft -- attitude stabilisation -- sampled-data control -- prediction mechanism -- H∞ performance; System analysis -- Periodicals; 003.3
• DOI: 10.1080/00207721.2017.1316883
• Languages: English
• ISSNs: 0020-7721

Abstract

ABSTRACT: This paper investigates the H ∞ control problem of the attitude stabilisation of a rigid spacecraft with external disturbances using prediction-based sampled-data control strategy. Aiming to achieve a 'virtual' closed-loop system, a type of parameterised sampled-data controller is designed by introducing a prediction mechanism. The resultant closed-loop system is equivalent to a hybrid system featured by a continuous-time and an impulsive differential system. By using a time-varying Lyapunov functional, a generalised bounded real lemma (GBRL) is first established for a kind of impulsive differential system. Based on this GBRL and Lyapunov functional approach, a sufficient condition is derived to guarantee the closed-loop system to be asymptotically stable and to achieve a prescribed H ∞ performance. In addition, the controller parameter tuning is cast into a convex optimisation problem. Simulation and comparative results are provided to illustrate the effectiveness of the developed control scheme.