An integrated control scheme for space robot after capturing non-cooperative target

被引:37
作者
Wang, Mingming [1 ,2 ]
Luo, Jianjun [1 ,2 ]
Yuan, Jianping [1 ]
Walter, Ulrich [3 ]
机构
[1] Northwestern Polytech Univ, Sci & Technol Aerosp Flight Dynam Lab, Xian 710072, Shaanxi, Peoples R China
[2] Northwestern Polytech Univ Shenzhen, Res Inst, Shenzhen 518057, Peoples R China
[3] Tech Univ Munich, Inst Astronaut, D-85748 Garchirtg, Germany
基金
中国国家自然科学基金;
关键词
Space robot; Detumbling strategy; Impedance control; Parameter identification; Post-capture; MOTION; STABILIZATION;
D O I
10.1016/j.actaastro.2018.04.016
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
How to identify the mass properties and eliminate the unknown angular momentum of space robotic system after capturing a non-cooperative target is of great challenge. This paper focuses on designing an integrated control framework which includes detumbling strategy, coordination control and parameter identification. Firstly, inverted and forward chain approaches are synthesized for space robot to obtain dynamic equation in operational space. Secondly, a detumbling strategy is introduced using elementary functions with normalized time, while the imposed end-effector constraints are considered. Next, a coordination control scheme for stabilizing both base and end-effector based on impedance control is implemented with the target's parameter uncertainty. With the measurements of the forces and torques exerted on the target, its mass properties are estimated during the detumbling process accordingly. Simulation results are presented using a 7 degree-of-freedom kinematically redundant space manipulator, which verifies the performance and effectiveness of the proposed method.
引用
收藏
页码:350 / 363
页数:14
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