中国空间科学技术

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轨道机动期间的姿态控制

吕振铎   

  1. 北京控制工程研究所
  • 发布日期:1994-10-25

ATTITUDE CONTROL DURING ORBIT MANEUVER

Lu Zhenduo(Beijing Institute of Control Engineering, Beijing 100080)   

  • Online:1994-10-25

摘要: 论述了轨道机动期间的姿态控制的一般原则,以及对不同稳定方式的卫星姿态控制的要求,文章着重分析了三轴稳定卫星控制系统设计的关键技术问题。

关键词: 轨道机动, 姿态控制, 稳定性, 灵敏度

Abstract: he paper discusses a general principle of attitude control during orbit maneuver.The attitude control requirements are different for two stabilized modes of a satellite.The paper emphatically analyses key teehnological problems on the control system design of three axis stabilized satellite during orbit maneuver.