| 地球同步卫星远地点变轨期间的三轴姿态稳定 |
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| 引用本文： | 周文忠.地球同步卫星远地点变轨期间的三轴姿态稳定[J].航天控制,1993(2). |
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| 作者姓名： | 周文忠 |
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| 作者单位： | 北京控制工程研究所 |
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| 摘 要： | 本文提供了地球同步三轴稳定卫星在远地点变轨机动过程中的卫星动力学模型,其中考虑了刚体、液体晃动和帆板振动的耦合,这些模型经过实际工程验证,证明是正确的。本文还给出了控制器结构,它由PID和各种晃动滤波器及帆板挠性滤波器组成。工程设计证明,这种控制器结构可满足设计要求且简单可靠。本文还给出了系统稳定性分析结果及数字仿真结果。
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| 关 键 词： | 太阳帆 柔性 三轴稳定 |
Three Axes Attitude Stabilization of Geostationary Satellite during Apogec orbit Maneuvering |
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| Zhou Wenzhong Beijing Institute of Control Engineering.Three Axes Attitude Stabilization of Geostationary Satellite during Apogec orbit Maneuvering[J].Aerospace Control,1993(2). |
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| Authors: | Zhou Wenzhong Beijing Institute of Control Engineering |
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| Institution: | Zhou Wenzhong Beijing Institute of Control Engineering |
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| Abstract: | A dynamics model including rigid, liquid sloshing and flexible solar array dynamics of three axis stabilized geostationary satellite during apogee orbit maneuver is provided in the paper. The model has proved valid pass through the practice satellite control design. A Type of controller which is consisted by PID. plexible solar array filters and sloshing filters is given. The design specification has been satisficed by the controller, and it is simple and reliable. Finally simulation and stability analysis results are provided. |
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| Keywords: | Solar array Flexibility Three axes stabilization |
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