| 某型防空导弹自适应自动驾驶仪设计 |
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| 引用本文： | 李云,刘兴堂,杨遵.某型防空导弹自适应自动驾驶仪设计[J].弹箭与制导学报,2006,26(2):27-29. |
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| 作者姓名： | 李云 刘兴堂 杨遵 |
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| 作者单位： | 空军工程大学导弹学院,陕西,三原,713800 |
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| 摘 要： | 采用模型参考自适应控制理论中的Popov超稳定性方法,设计了某防空导弹的自适应自动驾驶仪,进行了数字仿真,给出了仿真结果,得出了结论.
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| 关 键 词： | 模型参考自适应控制 超稳定性理论 防空导弹 自动驾驶仪 |
| 收稿时间： | 2006-03-20 |
| 修稿时间： | 2006年3月20日 |
Adaptive Autopilot Design for Air Defense Missile |
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| LI Yun,LIU Xing-tang,YANG Zun.Adaptive Autopilot Design for Air Defense Missile[J].Journal of Projectiles Rockets Missiles and Guidance,2006,26(2):27-29. |
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| Authors: | LI Yun LIU Xing-tang YANG Zun |
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| Affiliation: | The Missile Institute, Airforce Engineering University, Shaanxi Sanyuan 713800, China |
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| Abstract: | An approach of Popov hyperstability for model reference adaptive control theory was adopted. An adaptive autopilot for air defense missile was designed. Digital simulation was made and the result was presented. Finally, some conclusion was given out. |
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| Keywords: | model reference adaptive eontrol hyperstability theory air defense missile autopilot |
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