The Control Method of Force Loading of Robot on Load Transfer Mechanism of Space Station

Zhigang Xu, Xinlin Bai, Junyi Wang, Mingyang Liu, Xiao Zhang
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引用次数: 5

Abstract

when the robot loads force on space station transfer mechanism, there exist some issues such as unstable robot force control system, insufficient load accuracy, and long settling time. To solve these problems, a strategy for adjusting the admittance controller parameters adaptively is proposed. Firstly, the relationship between force and position is established according to the admittance control theory. And a force tracking/force loading controller based on the rectangular coordinate system is initially designed. Then, the parameters of the load transfer mechanism model are identified based on the loading experiment data by the least square method, and the relationship between force and position of robot in specific workspace is established. Finally, the parameters of the admittance controller are adaptively adjusted to make the robot dynamics model approximately match with the dynamic model of the load transfer mechanism. The real-time spatial loading force imposed by the robot on the end of the load transfer mechanism after spreading is realized. The experiment shows that the tracking error of the robot relative to the load transfer mechanism is less than 0.1 mm, and the loading force error is less than 1%, and the robot meets the requirement and provides a real equivalent space load for the space station transfer mechanism.
空间站载荷传递机构上机器人受力的控制方法
机器人在空间站传递机构上加载力时,存在机器人力控制系统不稳定、加载精度不足、沉降时间长等问题。针对这些问题,提出了一种自适应调整导纳控制器参数的策略。首先,根据导纳控制理论建立了力与位置的关系。并初步设计了基于直角坐标系的力跟踪/力加载控制器。然后,基于载荷实验数据,采用最小二乘法识别载荷传递机构模型参数,建立机器人在特定工作空间内受力与位置的关系;最后,自适应调整导纳控制器的参数,使机器人的动力学模型与负载传递机构的动力学模型近似匹配。实现了机器人在展开后对载荷传递机构端部施加的实时空间载荷力。实验表明,该机器人相对于载荷传递机构的跟踪误差小于0.1 mm,载荷力误差小于1%,满足要求,为空间站传递机构提供了真实的等效空间载荷。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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