A force and moment compensation method for a hardware-in-the-loop docking simulator based on the stiffness identification of the docking mechanism

被引:6
作者
Hu, Yan [1 ]
Gao, Feng [1 ]
Qi, Chenkun [1 ]
Zhao, Xianchao [1 ]
Wang, Qian [1 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Mech Engn, State Key Lab Mech Syst & Vibrat, Shanghai 200240, Peoples R China
基金
中国国家自然科学基金;
关键词
Hardware-in-the-loop simulation; Docking simulator; Force compensation; Stiffness identification; Contact dynamics; Divergence; DELAY-TIME COMPENSATION; CONTACT; VERIFICATION; SPACECRAFT;
D O I
10.1016/j.mechatronics.2021.102513
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A hardware-in-the-loop (HIL) docking simulator is an important validation facility on the ground for space docking. To reproduce the space docking process, the HIL docking simulator needs to solve the simulation distortion problem. In this paper, a force and moment compensation approach is presented to achieve a highfidelity HIL simulation for a six degree-of-freedom docking simulator. The whole loop in the HIL simulation is thoroughly analyzed, and the sources that lead to the distortion are illustrated. The force and moment compensation method considers the distortion sources from the time lag of the force sensor, the motion lag of the motion simulator and especially the deformation of the simulator mechanical structure. One key step in the force and moment compensation is the stiffness identification of the docking mechanism. The stiffness relationship among the whole system stiffness, the stiffness of the docking mechanism, and the structural stiffness of the simulator, is established. A stiffness identification model is deduced to obtain the stiffness of the docking mechanism from the whole system stiffness by excluding the structural stiffness of the simulator in real-time. The experimental results show the proposed compensation method can achieve a high-fidelity simulation for the docking simulator.
引用
收藏
页数:11
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