| 空间飞行器开关姿态系统的变结构模型跟随控制 |
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| 引用本文： | 戴学丰.空间飞行器开关姿态系统的变结构模型跟随控制[J].航天控制,1992(1). |
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| 作者姓名： | 戴学丰 |
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| 作者单位： | 哈尔滨船舶工程学院航天工程系 |
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| 摘 要： | 本文设计了某空间飞行器开关姿态控制系统的变结构模型参考控制器,该控制器结构简单并且使系统具有较强的鲁棒性,采用继电控制后系统具有良好的快速性及对常值干扰稳态误差为零。
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| 关 键 词： | 航天器 自适应控制 非线性系统 姿态控制 |
VARIABLE STRUCTURE MODEL-FOLLOWING CONTROL OF SWITCHING ATTITUDE SYSTEM OF SPACECRAFT |
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| Dai Xuefong.VARIABLE STRUCTURE MODEL-FOLLOWING CONTROL OF SWITCHING ATTITUDE SYSTEM OF SPACECRAFT[J].Aerospace Control,1992(1). |
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| Authors: | Dai Xuefong |
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| Institution: | Dai Xuefong Department of Astronautics Engineering Harbin Shipbuilding Engineering Institute |
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| Abstract: | A variable structure model-following odaptive controller for switching attitude system of some spacecraft is designed in this paper. The structure of the controller is simple and the robustness of a system ean be improved with the controller. After using bang-bang control, a rapid system response and zero steady-state error for constant disturbance can be obtained. |
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| Keywords: | Subject terms Spacecraft Adaptive control Nolinear system Attitude control |
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