嫦娥一号卫星的地月转移变轨控制  

Orbit Maneuver Control during Cislunar-Transfer Phase for CE-1 Spacecraft

作　　者：宗红[1] 王淑一[1] 韩冬[1] 王大轶[1] 李铁寿[1] 张洪华[1] 黄江川[1] 

机构地区：[1]北京控制工程研究所,北京100080

出　　处：《空间控制技术与应用》2008年第1期44-50,共7页Aerospace Control and Application

摘　　要：文章阐述了嫦娥一号卫星地月转移阶段(从星箭分离到进入使命轨道)的高可靠、高精度自主变轨控制方案,介绍了飞行轨道、轨控策略及控制参数优化、星上自主变轨控制的系统设计和相关参数的地面标定等,给出了在轨飞行试验的验证结果。A highly reliable and accurate on-board control system design scheme is presented for the orbit maneuvers of CE-1 spacecraft during its cislunar transfer phase. Flight trajectories, orbit transfer strategies and parameter optimization, on-board autonomous maneuver control procedures and parameter caliberations are addressed. Flight verification results are given as well.

关 键 词：嫦娥一号卫星 地月转移 轨道控制 自主变轨控制 

分 类 号：V446.1[航空宇航科学与技术—飞行器设计] V448.22