Adaptive sliding mode disturbance observer-based control for rendezvous with non-cooperative spacecraft

被引:28
|
作者
Zhu, Xiaoyu [1 ,2 ]
Chen, Junli [1 ]
Zhu, Zheng H. [2 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, 800 Dongchuan Rd, Shanghai 200240, Peoples R China
[2] York Univ, Dept Mech Engn, 4700 Keele St, Toronto, ON M3J 1P3, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Non-cooperative spacecraft; Rendezvous; Orbital dynamics; Adaptive sliding mode; Disturbance observer; FINITE-TIME CONTROL; PROXIMITY OPERATIONS; ATTITUDE-TRACKING; COORDINATION CONTROL; ROBUST-CONTROL; DOCKING; POSITION;
D O I
10.1016/j.actaastro.2021.03.005
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper investigates the tracking and control problem of a spacecraft rendezvous with a non-cooperative and tumbling space target subject to parametric uncertainty and unknown external disturbances. The kinematics and dynamics of spacecraft position and attitude are described by dual quaternions. A novel adaptive sliding mode disturbance observer is proposed to track the pose of non-cooperative tumbling target without need for upper bounds of first and second derivatives of lumped disturbance. Based on the proposed observer, a finite time sliding mode control is developed in term of dual quaternion. Different from existing sliding mode control schemes, the conditions on the controller parameters bounds are relaxed. The stability and robustness of the overall closed-loop control is proved by the Lyapunov framework. The robustness and effectiveness of the proposed control scheme are validated by numerical simulations in comparison with existing approaches.
引用
收藏
页码:59 / 74
页数:16
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