| 导弹非线性系统的飞行控制 |
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| 引用本文： | 顾文锦,赵国荣.导弹非线性系统的飞行控制[J].战术导弹技术,1996(3):33-38. |
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| 作者姓名： | 顾文锦 赵国荣 |
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| 作者单位： | 海军航空工程学院，海军航空工程学院 |
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| 摘 要： | 文献1,2]给出了块对角非线性系统相对度分解设计理论和导弹的块对角控制器。为解决某型反舰导弹诸问题,进行了大量的数学仿真,并与该导弹原控制系统的仿真结果作了对比。
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| 关 键 词： | 导弹 非线性系统 控制 飞行仿真 |
FLIGHT CONTROL ON NONLINEAR SYSTEM OF A MISSILE |
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| Gu Wenjin Zhao Guorong Naval Aeronautical Engineering Academy.FLIGHT CONTROL ON NONLINEAR SYSTEM OF A MISSILE[J].Tactical Missile Technology,1996(3):33-38. |
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| Authors: | Gu Wenjin Zhao Guorong Naval Aeronautical Engineering Academy |
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| Affiliation: | Gu Wenjin Zhao Guorong Naval Aeronautical Engineering Academy |
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| Abstract: | A theory of relative-degree decomposition of nonlinear system and a block diagonal controller of a missile are given in Ref.1,2].To solve some problems of certain anti-ship missile,st lot of mathematical simulations,are carried out.The calculated results are compared with old system's one. |
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| Keywords: | Nonlinear systems Control Flight simulation |
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