| 基于鲁棒控制方法的卫星姿态控制 |
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| 引用本文： | 马克茂,伞冶. 基于鲁棒控制方法的卫星姿态控制[J]. 航天控制, 2001, 19(4): 29-34 |
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| 作者姓名： | 马克茂 伞冶 |
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| 作者单位： | 哈尔滨工业大学仿真中心,哈尔滨,150001 |
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| 摘 要： | 针对卫星姿态控制系统 ,建立了简化的线性数学模型 ,利用鲁棒控制方法设计了卫星姿态控制律 ,由于在设计中考虑了建模过程中的简化而带来的不确定性 ,因而基于线性模型所设计的控制律能够应用于非线性卫星姿态系统的控制
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| 关 键 词： | 卫星 姿态控制 鲁棒控制 主动控制 |
| 修稿时间： | 2001-03-19 |
Attitude Control of Satellite Based on Robust Control Method |
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| Ma Kemao San Ye Simulation Center,Harbin Institute of Technology,Harbin. Attitude Control of Satellite Based on Robust Control Method[J]. Aerospace Control, 2001, 19(4): 29-34 |
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| Authors: | Ma Kemao San Ye Simulation Center Harbin Institute of Technology Harbin |
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| Affiliation: | Ma Kemao San Ye Simulation Center,Harbin Institute of Technology,Harbin,150001 |
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| Abstract: | Simplified linear mathematical model of satellite attitude control system is constructed, based on which attitude control law is designed using robust control theory. As simplifications in model construction are considered during design, the obtained control law based on simplified model is applicable to nonlinear satellite attitude system. |
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| Keywords: | Satellite Attitude control Robust control Active control |
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