| 巡航导弹地形跟踪Wiener-Hopf最优控制器设计研究 |
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| 引用本文： | 李冬梅,刘俊强,胡恒章.巡航导弹地形跟踪Wiener-Hopf最优控制器设计研究[J].航天控制,1998,16(3):30-35. |
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| 作者姓名： | 李冬梅 刘俊强 胡恒章 |
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| 作者单位： | 哈尔滨工业大学控制工程系,150001 |
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| 摘 要： | 为了提高巡航导弹的生存能力，使其能够跟踪地形起伏飞行，提出了用二自由度Ｗｉｅｎｅｒ－Ｈｏｐｆ最优化方法设计地形跟踪控制器。仿真结果表明，该方法具有良好的跟踪性能。另外，针对反馈通道气压式高度表的延迟问题，提出了气压—惯性方案，并进行了仿真验证。
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| 关 键 词： | 最佳控制 控制器 地形跟踪 |
| 修稿时间： | 1997年10月18日 |
Study of Wiener - Hopf Optimal Controller Design for Terrain Following System of Cruise Missile |
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| Li Dongmei,Liu Junqiang,Hu Hengzhang.Study of Wiener - Hopf Optimal Controller Design for Terrain Following System of Cruise Missile[J].Aerospace Control,1998,16(3):30-35. |
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| Authors: | Li Dongmei Liu Junqiang Hu Hengzhang |
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| Institution: | Li Dongmei\ Liu Junqiang\ Hu Hengzhang Department of Control Engineering Harbin Institute of Technology 150001 |
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| Abstract: | Adopts two-degree-of-freedom Wiener-Hopf optimal method to design a cruise missile's terrain following controller, in order to improve its viability. The simulation results evince that the offered method has a favourable terrain following performance. And presents an altimeter-inertia scheme, which is validated by simulation, to deal with the time delay of baric altimeter in feedback loop. |
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| Keywords: | Optimal control\ Controller\ Terrain following |
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