| 挠性卫星姿态运动的鲁棒控制技术 |
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| 引用本文： | 陈亚陵.挠性卫星姿态运动的鲁棒控制技术[J].厦门大学学报(自然科学版),2001,40(2):211-219. |
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| 作者姓名： | 陈亚陵 |
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| 作者单位： | 厦门大学自动化系, |
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| 基金项目： | 中国空间技术研究院"九五"预研重点课题(无编号) |
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| 摘 要： | 具有挠性振动和液体晃动的新一代挠性卫星姿态运动是一个不确定系统,运用H∞优化与μ综合技术研究具有抑制振动和晃动能力以及强鲁棒性的卫星姿态控制系统设计问题,并对所提出的几种鲁棒控制系统设计方案进行计算机仿真和全物理仿真实验研究。
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| 关 键 词： | 卫星姿态运动 鲁棒控制 挠性振动 回路成形 物理仿真 液体晃动 姿态控制 航天技术 |
| 文章编号： | 0438-0479(2001)02-0211-09 |
| 修稿时间： | 2001年2月15日 |
Robust Control Technigue of Flexible Satellite Attitude Movement |
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| Chen Ya-ling.Robust Control Technigue of Flexible Satellite Attitude Movement[J].Journal of Xiamen University(Natural Science),2001,40(2):211-219. |
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| Authors: | Chen Ya-ling |
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| Abstract: | Attitude movement of new style flexible satellite is uncertain systems. The control system design problem with the suppession of the flexible structure vibration and the liquid slosh ing as well as the strong robustness was studied by using H∞ optimal method and μ synthesis technigue. The computer simulation and physical simulation experiment were also studied for some robust control schemes. |
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| Keywords: | satellite attitude robust control flexible vibration loop shaping physical simula-tion |
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