摘要
空间寻的轨道交会中,传统的C-W交会在目标航天器轨道为圆形时能顺利完成交会任务,但当目标航天器作一般的椭圆轨道运动时,C-W方法失效,而本文提出的一种改进的C-W交会方法适用于一般的椭圆轨道交会。本文对这两种方法进行了比较分析,并进行了数学仿真研究,仿真结果表明了改进的C-W交会的有效性。
The traditional C-W method is useful for circular orbits in spacecraft rendezvous, but it is invalid when the target spacecraft moving on the elliptical orbit. While the improved C-W method introduced in this article is adaptable to general elliptical orbit. The two methods are analyzed and the relative computer simulations are carried out as well. The simulation result verifies the validity of the improved C-W method.
出处
《航天控制》
CSCD
北大核心
2009年第5期28-30,共3页
Aerospace Control
