摘要
Space robots have attracted increasing attention for performing, autonomously or telerobotically, on-orbit servicing missions such as repairing, refueling, and upgrading spacecraft; reusing space assets; and on-orbit assembly. The extension of robot application to space can release astronauts from risky, time-consuming, and expensive extravehicular activities [1]. However, in the microgravity environment, the floating base of a space robot will be disturbed by the robot's arm motion when it approaches or manipulates a target. The motion of the spacecraft base resulting from this disturbance will, conversely, affect the motion of end effectors (known as coupling dynamics), making control of space robots more complicated than that of fixed-base robots. In addition, such a disturbance of spacecraft attitude may result in a communication interruption between the spacecraft and the ground station or a failure of energy accumulation caused by disorientation of solar panels [2].
| 源语言 | 英语 |
|---|---|
| 期刊论文编号 | 8472216 |
| 页(从-至) | 86-95 |
| 页数 | 10 |
| 期刊 | IEEE Robotics and Automation Magazine |
| 卷 | 25 |
| 期 | 4 |
| DOI | |
| 出版状态 | 已出版 - 12月 2018 |
学术指纹
探究 'Coordinated Control of a Dual-Arm Space Robot: Novel Models and Simulations for Robotic Control Methods' 的科研主题。它们共同构成独一无二的学术指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver