摘要
导出了基于相对轨道要素的编队飞行卫星群轨道相对运动控制的轨道机动方程 ;提出了编队飞行卫星群轨道相对运动控制的轨道机动控制策略 ,利用不同方向的脉冲控制相对运动的轨道参数 ,包括轨道平面内机动和轨道平面外机动控制。根据相对轨道要素的变轨机动控制 ,进行编队飞行卫星群构型的初始化。这样的构型初始化可以视作一次特殊的变轨机动控制 。
This paper deduces the orbit maneuver equations for relative motion control of satellite formations based on the relative orbit elements. It proposes orbit maneuver control methods for relative orbital motion control of satellite formations, including the maneuver control both in and out of the orbit plane, based on orbit parameters of relative motion controlled by pulses in different directions. The configuration initialization of satellite formations is carried out based on orbit maneuver control of relative elements. This orbit initialization can be considered as a special kind of orbit maneuver control. This procedure in easily realized for initialization of satellite formations .
出处
《中国空间科学技术》
EI
CSCD
北大核心
2003年第2期51-57,共7页
Chinese Space Science and Technology
基金
国家自然科学基金资助项目 ( 10 0 82 0 0 1)
