| 三轴定向充液卫星的姿态稳定性 |
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| 引用本文： | 包光伟,刘延柱.三轴定向充液卫星的姿态稳定性[J].空间科学学报,1993,13(1):31-38. |
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| 作者姓名： | 包光伟 刘延柱 |
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| 作者单位： | 上海交通大学工程力学系 200030
(包光伟)，上海交通大学工程力学系 200030(刘延柱) |
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| 摘 要： | 本文建立了三轴定向充液卫星具有二维平动和二维摆动角的等效力学模型,并用该模型研究了充液卫星的姿态稳定性,得到了充液系统姿态稳定性的一个简明的解析判据。
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| 关 键 词： | 液体晃动 姿态稳定性 卫星 动力学 |
THE ALTITUDE STABILITY OF THREE-AXIS LIQUID FILLED SATELLITE |
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| Bao Guang-wei Liu Yan-zhu.THE ALTITUDE STABILITY OF THREE-AXIS LIQUID FILLED SATELLITE[J].Chinese Journal of Space Science,1993,13(1):31-38. |
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| Authors: | Bao Guang-wei Liu Yan-zhu |
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| Abstract: | This paper set up the equivalent mechanical model of the three-axis liquid filled satellite which has both translational and pitch-yaw disturbance. Then, using this model, the altitude stability of the satellite is investigated and a coincise analytic criterion is obtained. |
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| Keywords: | Liquid sloshing Equivalent mechanical model Altitude stability |
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