| 最优控制与姿控喷流在导弹姿态控制中的应用 |
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| 引用本文： | 林枫,刘国刚. 最优控制与姿控喷流在导弹姿态控制中的应用[J]. 航天控制, 2004, 22(3): 20-22 |
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| 作者姓名： | 林枫 刘国刚 |
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| 作者单位： | 上海机电工程研究所,上海,200233;上海机电工程研究所,上海,200233 |
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| 摘 要： | 针对稀薄大气层内导弹姿态控制问题 ,提出了一种采用侧向喷流的姿态控制方案 ,并根据最优控制理论设计了控制律。仿真结果表明 ,该方案可以在最短的时间内使导弹的姿态跟踪给定的指令输入 ,并且具有较小的稳态误差
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| 关 键 词： | 最优控制 Bang-Bang控制 姿控喷流 偏航角 开关线 |
| 文章编号： | 1006-3242(2004)03-20-03 |
| 修稿时间： | 2004-01-15 |
Application of Optimal Control Using Direct Side Force in Missile Attitude Control System |
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| Lin Feng Liu Guogang Shanghai Electro-Mechanical Engineering Institute,Shanghai. Application of Optimal Control Using Direct Side Force in Missile Attitude Control System[J]. Aerospace Control, 2004, 22(3): 20-22 |
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| Authors: | Lin Feng Liu Guogang Shanghai Electro-Mechanical Engineering Institute Shanghai |
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| Affiliation: | Lin Feng Liu Guogang Shanghai Electro-Mechanical Engineering Institute,Shanghai 200233 |
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| Abstract: | In this paper, attitude control system ap pl ying direct side force nozzle is presented as a measure to realize missile attit ude control in attenuate aerosphere, and a control law is designed. Simulation r esult indicates that missile attitude response could track command in the least time, and had small steady state error. < |
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| Keywords: | Optimal control Bang-Bang control Direct Side Force Yawing angle Switch cur ve |
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