| 同步卫星姿态控制系统稳定性分析 |
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| 引用本文： | 周伯昭.同步卫星姿态控制系统稳定性分析[J].航天控制,1990(3). |
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| 作者姓名： | 周伯昭 |
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| 作者单位： | 国防科学技术大学 |
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| 摘 要： | 本文介绍苏联“萤光屏”系列地球同步卫星的姿态控制系统以及在稳态运行时姿态控制系统俯仰通道的稳定性分析,分析中考虑了太阳帆板的挠性。飞行实验表明,文中所介绍的方法在工程设计中是简单可行的。
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| 关 键 词： | 同步卫星 姿态控制系统 挠性帆板 稳定性分析 |
STABILITY ANALYSIS OF ATTITUDE CONTROL SYSTEM OF SYNCHRONOUS SATELLITE |
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| Zhou Bozhao National University of Defense Technology.STABILITY ANALYSIS OF ATTITUDE CONTROL SYSTEM OF SYNCHRONOUS SATELLITE[J].Aerospace Control,1990(3). |
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| Authors: | Zhou Bozhao National University of Defense Technology |
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| Institution: | Zhou Bozhao National University of Defense Technology |
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| Abstract: | In this paper, the attitude control system of the earth-synchronous satellite and stability analysis of its pitch loop are presented. The flexibility of solar array is included in this analysis. Flight experiments demonstrate that the analysis method is simple and feasible in engineering design. |
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| Keywords: | Synchronous satellite Attitude control system Flexible solar array Stability analysis |
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