摘要
本文在文[2]、[4]的基础上,研究了最优交会轨道,导出了在推力作用下最优交会轨道的解析表达式;并对最优交会轨道和最优控制规律作了数值计算,求得了最优解。结果表明,对于目标航天器绕圆形轨道运行的情况,要求最优空间交会轨道和最省燃料的控制规律,此法有较好的实用价值。
This paper studies the optimal orbit of rendezvous on the basis of references [2], [4], deduces the analytical expression of the optimal orbit of rendezvous under the action of thrust, makes numerical calculations and obtains the solutions for the optimal orbit of rendezvous and the optimal rules of control. The results show that this method has good practical value for finding out the optimal orbit of rendezvous in space and the rules of the most fuel saving control in the circumstances of target spaceflighter moving in round orbit.
关键词
航天飞机
轨道
最优交会
控制
space shuttle, orbits, optimization, optimal rendezvous orbits, fuel control
