An enhanced anti-disturbance attitude control law for flexible spacecrafts subject to multiple disturbances. (March 2019)

• Record Type: Journal Article
• Authors: Zhu, Yukai; Guo, Lei; Qiao, Jianzhong; Li, Wenshuo
• Is Part Of: Control engineering practice. Volume 84(2019)
• Page Start: 274
• Page End: 283
• Publication Date: 2019-03
• Subjects: Flexible spacecrafts -- Multiple disturbances -- Enhanced anti-disturbance control -- Disturbance observer-based control -- Active disturbance rejection control; Automatic control -- Periodicals; 629.89
• DOI: 10.1016/j.conengprac.2018.11.001
• Languages: English
• ISSNs: 0967-0661

Abstract

Abstract: As well-known disturbance rejection methods, active disturbance rejection control and disturbance observer-based control can effectively improve the control performances of complex systems in the presence of disturbances. However, the accurate rejection of multiple disturbances for control systems of practical engineering, for example, the attitude control system of flexible spacecraft, is still a bottleneck problem. In order to further improve the anti-disturbance capability and reduce the conservativeness, this paper proposes a novel enhanced anti-disturbance control law for the attitude control system of flexible spacecraft by combining active disturbance rejection control and disturbance observer-based control in a unified framework. More specifically, the disturbance from flexible vibration is described by an uncertain exogenous system based on the partially known information including elastic damping ratios and modal frequencies. The disturbance observer-based control is utilized to estimate and thereby reject this disturbance. On the other hand, the other disturbances such as external environmental disturbance and complex model nonlinearity are merged into a equivalent disturbance with bounded derivative, which is compensated by using the active disturbance rejection control law. Stability and robustness analysis are carried out for the disturbance observer and extended state observer. Finally, simulation results of low-earth-orbit flexible satellite are presented to verify the effectiveness of proposed methods.