| 大型挠性空间结构的变结构控制 |
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| 引用本文： | 熊勇,吴宏鑫.大型挠性空间结构的变结构控制[J].航天控制,1996(3). |
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| 作者姓名： | 熊勇 吴宏鑫 |
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| 作者单位： | 北京控制工程研究所 |
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| 摘 要： | 本文从ＬＦＳＳ的相对阶为２的特点出发设计了用于ＬＦＳＳ的镇定控制的变结构控制器,从而避免了主导极点的选择（模态截断）,解决了“控制溢出”问题。以太阳帆板展开过程中航天器姿态控制为例,作了计算机仿真。
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| 关 键 词： | 航天器 挠性结构 姿态控制 |
Variable Structure Control of Large Flexible Space Structure |
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| Xiong Yong ,Wu Hongxin.Variable Structure Control of Large Flexible Space Structure[J].Aerospace Control,1996(3). |
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| Authors: | Xiong Yong Wu Hongxin |
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| Institution: | Beijing institute of Control Engineering 100080 |
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| Abstract: | This paper presents a kind of VSC to stabilize LFSS based on the relative order of LFSS equal to 2, if avoids the selection of major poles and solves the problem of " control spillover". Finally. satellite attitude control during deployment solar panels as an example, simulation on computer is performed. |
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| Keywords: | Spacecraft Flexible structure Attitude control |
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