中国空间科学技术Issue(2)：69-75,7.DOI:10.3780/j.issn.1000-758X.2014.02.009
编队飞行相对倾斜构形的 e／i矢量控制方法
Control Method Based On e/i Vector to Realize Satellites Formation with Relative Inclined Configuration
伍升钢 1钱山 2李恒年 1谭炜2
作者信息
- 1. 宇航动力学国家重点实验室，西安 710043
- 2. 中国西安卫星测控中心，西安 710043
- 折叠
摘要
Abstract
The problem of relative inclined configuration design and orbit control of the distributed InSAR satellites formation flying was studied . First , the algorithm of relative inclined configuration design based on e/i vector was put forward . Then the relationship between the relative inclined configuration and the errors of eccentricity , inclination and the right ascension of ascending node were given . According to the properties of relative inclined configuration of distributed satellites , the four-impulse orbit maneuver strategy was put forward based on the Gauss perturbation functions satellite formation control model . Simulation results show that the method of relative inclined configuration design is intuitionistic , the orbit maneuver strategy is simple and the configuration is stable .关键词
分布式卫星/e/i矢量/相对倾斜构形/绕飞角/轨道控制Key words
Distributed satellites/e/i vector/Relative inclined configuration/Flying-around angle/Orbit control引用本文复制引用
伍升钢,钱山,李恒年,谭炜..编队飞行相对倾斜构形的 e／i矢量控制方法[J].中国空间科学技术,2014,(2):69-75,7.
