| 航天器太阳帆板展开过程的最优控制 |
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| 引用本文： | 戈新生 刘延柱. 航天器太阳帆板展开过程的最优控制[J]. 空间科学学报, 1997, 17(4): 360-366. DOI: 10.11728/cjss1997.04.360 |
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| 作者姓名： | 戈新生 刘延柱 |
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| 作者单位： | 1.北京机械工业学院基础部 100085 |
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| 摘 要： | 本文讨论航天器太阳帆板展开过程中主体姿态的最优控制问题. 利用多体动力学与最优控制理论建立数学模型, 考虑系统的非完整约束特性, 提出太阳帆板展开过程的最优控制算法. 通过数值仿真, 表明该方法对太阳帆板展开姿态控制的有效性.
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| 关 键 词： | 多体动力学 最优控制 姿态控制 太阳帆板展开 |
| 收稿时间： | 1996-10-23 |
OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR WINGS ON SPACECRAFT |
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| GE Xinsheng. OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR WINGS ON SPACECRAFT[J]. Chinese Journal of Space Science, 1997, 17(4): 360-366. DOI: 10.11728/cjss1997.04.360 |
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| Authors: | GE Xinsheng |
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| Affiliation: | 1.Basic Science Courses Department, Beijing Institute of Machinery Industry 1000852.Department of Engineering Mechanics, Shanghai Jiao Tong University |
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| Abstract: | The optimal attitud control problem of speecraf during the sbetehing Process ofsolar wings is discussed in mis paper A mathematical model of the systom isestabished by use of the mulhbody dynamics and oPtical control theory. An algorithmof contro for the stretching process is proposed, considering the nonhlonomic behaviorof the system. The effectiveness of the apprach is shown by numerical simulation. |
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| Keywords: | Mulhbody dynamics Optimal control Attitude control Stretching of solar wings |
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