| 轨道机动期间的姿态控制 |
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| 引用本文： | 吕振铎.轨道机动期间的姿态控制[J].中国空间科学技术,1994,14(5):25-30. |
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| 作者姓名： | 吕振铎 |
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| 作者单位： | 北京控制工程研究所 |
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| 摘 要： | 论述了轨道机动期间的姿态控制的一股原则，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。
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| 关 键 词： | 轨道机动 姿态控制 稳定性 灵敏度 航天器 |
ATTITUDE CONTROL DURING ORBIT MANEUVER |
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| Lu Zhenduo.ATTITUDE CONTROL DURING ORBIT MANEUVER[J].Chinese Space Science and Technology,1994,14(5):25-30. |
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| Authors: | Lu Zhenduo |
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| 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. |
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| Keywords: | rbit maneuver Attitude c ontrol Stability Sensibility Analyzing |
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