| 模型不确定的空间机器人无力传感器阻抗控制方法 |
| |
| 引用本文： | 陶东,张强,赵良玉. 模型不确定的空间机器人无力传感器阻抗控制方法[J]. 宇航学报, 2021, 42(6): 766-774. DOI: 10.3873/j.issn.1000-1328.2021.06.010 |
| |
| 作者姓名： | 陶东 张强 赵良玉 |
| |
| 作者单位： | 1. 北京理工大学宇航学院，北京100081；2. 北京控制工程研究所，北京100094 |
| |
| 基金项目： | 国家重点研发计划(2018AAA0103004）；国家自然科学基金（51805025，11532002) |
| |
| 摘 要： | 针对自由漂浮空间服务机器人在轨捕获时与服务对象的碰撞问题,提出一种考虑模型不确定情况下的无力传感器阻抗控制方法.通过将不确定模型观测的接触力和神经网络对模型不确定部分辨识得到的接触力,共同作为末端执行器与服务对象抓捕点的估计接触力和阻抗控制器的反馈,使空间机器人在模型不确定和无力传感器的情况下仍能实现与服务对象的柔性接...
|
| 关 键 词： | 空间机器人 无力传感器 阻抗控制 力估计 在轨捕获 |
| 收稿时间： | 2020-07-06 |
Force Sensorless Impedance Control for a Space Robot with Dynamic Uncertainty |
| |
| TAO Dong,ZHANG Qiang,ZHAO Liang yu. Force Sensorless Impedance Control for a Space Robot with Dynamic Uncertainty[J]. Journal of Astronautics, 2021, 42(6): 766-774. DOI: 10.3873/j.issn.1000-1328.2021.06.010 |
| |
| Authors: | TAO Dong ZHANG Qiang ZHAO Liang yu |
| |
| Affiliation: | 1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;2. Beijing Institute of Control Engineering, Beijing 100094, China |
| |
| Abstract: | A force sensorless impedance control approach is proposed for the collision between the free floating space robot and the captured object by taking the dynamic parameters uncertainty into account. The contact force identified by the neural network and the other contact force observed by the inaccurate dynamic model are both employed as the estimated contact force between the end effector and the target object as well as the feedback of the impedance controller. The method enables the space robot to flexibly capture the service object even if the dynamic parameters are uncertain and the force sensor is not assembled. The numerical simulation results show that this method can effectively reduce the requirement for the precision of space robot dynamics modeling and is practical in engineering. |
| |
| Keywords: | Space robot Sensorless Impedance control Force estimation On orbit capture |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《宇航学报》浏览原始摘要信息 |
|
点击此处可从《宇航学报》下载全文 |
