Observer-based control for the platform of a tethered space robot

被引:7
作者
Zhai, Guang [1 ]
Zheng, Heming [1 ]
Zhang, Bo [2 ]
机构
[1] Beijing Inst Technol, Aerosp Engn Sch, Beijing 100081, Peoples R China
[2] Aerosp Syst Engn Shanghai, Shanghai 201109, Peoples R China
基金
中国国家自然科学基金;
关键词
Adaptive control; Attitude dynamics; Disturbance observer; Sliding mode control; Tethered space robot; FLEXIBLE SPACECRAFT; DYNAMICS; DISTURBANCE; SATELLITE; TENSION; SYSTEMS; ORBITS; IMPACT; TASK;
D O I
10.1016/j.cja.2018.01.012
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper addresses the attitude control problem of a space tethered robot platform in the presence of unknown external disturbance caused by a connecting elastic tether. The tether-generated unknown disturbance leads to tremendous challenges for attitude control of the platform. In this work, the perturbed attitude dynamics of the platform are derived with a consideration of the libration of the elastic tether, and then with the purpose of compensating the unknown disturbance, major attention is dedicated to develop a nonlinear disturbance observer based on gyros measurements, after which, an adaptive attitude scheme is proposed by combining the disturbance observer with a sliding mode controller. Finally, benefits from the observer based on an adaptive controller are validated by series of numerical simulations. (C) 2018 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.
引用
收藏
页码:1786 / 1796
页数:11
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