Command-filtered incremental backstepping attitude control of spacecraft with predefined-time stability

被引:1
作者
Zhang, Haichao [1 ]
Huang, Haowei [2 ]
Xiao, Bing [1 ]
Dong, Kejun [1 ]
机构
[1] Northwestern Polytech Univ, Sch Automat, Xian 710072, Peoples R China
[2] CSG Guangdong Power Grid Corp, Guangzhou 510620, Guangdong, Peoples R China
关键词
Incremental backstepping control; Predefined-time stability; Spacecraft attitude control; Command filter; Disturbance observer; NONLINEAR DYNAMIC INVERSION; TRACKING CONTROL; FLIGHT CONTROL; CONTROL DRIVEN; SYSTEMS;
D O I
10.1016/j.ast.2024.109552
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper investigates the predefined-time attitude tracking control problem within the theoretical framework of incremental dynamic inversion. The utilization of the Taylor series facilitates the transformation of the attitude control system into a discrete-time plant, with the control input expressed in an incremental form. Additionally, a novel predefined-time stable dynamics system is presented and incorporated into the disturbance observer designing process, serving the purpose of estimating lumped disturbance. It is also employed in a command filter design to approximate the derivatives of the virtual control law within a predefined time. Consequently, an incremental backstepping attitude tracking control scheme is further developed, integrating the proposed predefined-time disturbance observer to ensure the system's robustness and the predefined-time filter to address challenges related to "term explosion" and singularity problem. Rigorous Lyapunov analysis affirms that the attitude control system, when using the incremental backstepping controller, remains predefined-time stable. The effectiveness of the proposed control scheme is subsequently validated through numerical simulations.
引用
收藏
页数:9
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