Approach Planning and Guidance for Uncontrolled Rotating Satellite Capture Considering Collision Avoidance
Approach Planning and Guidance for Uncontrolled Rotating Satellite Capture Considering Collision Avoidance
复制标题
DOI：
--
复制
发表时间：
2003
期刊：
影响因子：
--
通讯作者：
S. Matsumoto;S. Jacobsen;S. Dubowsky;Y. Ohkami
中科院分区：
文献类型：
--
作者：
S. Matsumoto;S. Jacobsen;S. Dubowsky;Y. Ohkami
研究了机器人捕获无控旋转卫星的安全运动学接近轨迹规划问题，提出了两种轨迹规划方法。第一种方法是利用轨道力学方程，针对目标卫星的某些运动条件，规划被动飞掠接近路径。第二种方法使用优化技术来规划相对于一组性能度量优化的接近轨迹。这些方法的代表性方案的结果，并讨论了每种方法的相对优点。1. 1.已证明使用机器人技术进行在轨卫星捕获，空间机器人技术今后可能在卫星服务飞行任务中发挥越来越大的作用。由航天飞机携带并由一名宇航员操作的航天飞机遥控操作系统（SRMS）已被使用
The problem of planning safe kinematic approach trajectories for robotic capture of an uncontrolled rotating satellite is addressed, and two methods of trajectory planning are presented. The first method uses equations of orbital mechanics to plan a passive fly-by approach path for certain conditions of target satellite motion. The second method uses optimization techniques to plan an approach trajectory that is optimized with respect to a set of performance metrics. Results of these methods for representative scenarios are presented, and the relative merits of each method are discussed. 1. Introduction The use of robotic technology for on-orbit satellite capture has been demonstrated and space robotics are likely to play an increasing role in satellite servicing missions in the future. The Shuttle Remote Manipulator System (SRMS), carried by the Space Shuttle and operated by an astronaut, has been used