Enhanced rapid attitude stabilization for space robots in postcapture using an iterated extended Kalman filter

被引:1
作者
Zhang, Teng [1 ]
Shi, Peng [1 ]
Guo, Ming [2 ]
Yue, Xiaokui [3 ,4 ]
机构
[1] Beihang Univ, Sch Astronaut, 37 Xueyuan Rd, Beijing, Peoples R China
[2] Chinese Acad Sci, Innovat Acad Microsatellites, 99 Haike Rd, Shanghai 201203, Peoples R China
[3] Northwestern Ploytechn Univ NWPU, Sch Astronaut, 127 Westyouyi Rd, Xian 710072, Shaanxi, Peoples R China
[4] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, 127 Westyoui Rd, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
Space robot; Rapid stabilization; Uncertainties; Extended Kalman filter; REACTIONLESS CONTROL; MANIPULATOR; TARGET;
D O I
10.1016/j.asr.2023.09.023
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Due to residual momentum, the space robot is tumbling after capturing an unknown target, like space debris because of the law of conservation of momentum. Therefore, it is essential to stabilize the attitude of the base for the objectives such as communication. In addition to the residual momentum and uncertainties in the inertial parameters of the target, the observation noise in real applications would degrade the stabilization performance or even lead to instability. To reduce the impacts of these factors, a novel strategy is presented in this paper for rapid attitude stabilization of space robots in postcapture. This approach exploits the dynamical coupling between the base and the manipulator to stabilize the attitude of the base with the limited control torque. In addition, to mitigate the effects of parameter and measurement uncertainties, an iterated extended Kalman filter is applied to estimate the motion state of the system and inertial parameters of the target in situations with state-dependent measurement noise. To verify the validity and feasibility of the presented approach, numerical simulations have been performed for the 2D and 3D models, and robustness and the effects of observation noise and initial velocity of the base have been analyzed via Monte Carlo simulations. (c) 2023 COSPAR. Published by Elsevier B.V. All rights reserved.
引用
收藏
页码:4965 / 4983
页数:19
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