| 卫星太阳阵展开的动力学方程 |
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| 引用本文： | 汪恩松. 卫星太阳阵展开的动力学方程[J]. 北京航空航天大学学报, 1994, 20(4): 446-451 |
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| 作者姓名： | 汪恩松 |
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| 作者单位： | 北京航空航天大学应用数理系 |
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| 摘 要： | 研究了卫星太阳阵展开的动力学问题，将卫星太阳阵的结构视为树形多体系统，利用给出的自由形式树形多刚体系统运动微分方程建立太阳阵系统的动力学方程，应用为该系统动力学方程编制的计算程序，可对太阳阵展开过程中卫星本体姿态的改变量以及太阳帆板在展开过程中的运动参数进行数值计算。
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| 关 键 词： | 刚体动力学 卫星 动力学方程 太阳阵 |
DYNAMICAL EQUATIONS FOR SOLAR WING |
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| Wang Ensong. DYNAMICAL EQUATIONS FOR SOLAR WING[J]. Journal of Beijing University of Aeronautics and Astronautics, 1994, 20(4): 446-451 |
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| Authors: | Wang Ensong |
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| Abstract: | This paper studies dynamics of satellite solar wing. which is a treeshaped multibody system. The dynamical equations for solor wing is established by means of dynamical equations for treeshaped multi-rigid-body systems which had been derived by author. In this paper the method for developing the software for simulation is given, which affords us to select optimal parameters of solar wing. |
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| Keywords: | rigid body kinetics satellites dynamical equations solar wing |
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