摘要
本文研究卫星编队重新配置机动中在碰撞避免约束条件下故障星离开编队以及备份星进入编队的轨迹规划及控制策略,研究表明选择机动的启动时刻不但能够构成所需要的编队构型,而且可以节省燃料、实现碰撞避免,以太阳同步轨道卫星编队为对象进行的仿真显示控制策略是简单、有效的。
With the constraint of collision avoidance, trajectory planning and cotrol for
satellite formation flying is presented by which fault satellite leaves the formation and new
satellite join in the formation. For saving the fuel and avoiding collision, the start time of
maneuver must be selected carefully. Then sun synchronization orbit satellite formation is sim-
ulated. The result of simulation demonstrates validity of control scheme.
出处
《航天控制》
CSCD
北大核心
2003年第4期11-17,共7页
Aerospace Control
