带落角和末端攻角约束的最优末制导律
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( 1.海军航空工程学院控制工程系,山东烟台 264001;2.海军航空工程学院研究生管理大队,山东烟台 264001)

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TJ765.3

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Optimal Guidance Law with Constrainton Terminal Impact Angle and Angle of Attack
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( 1.Naval Aeronautical and Astronautical University Department of Control Engineering, Yantai Shandong 264001, China;2.Naval Aeronautical and Astronautical University Graduate Students’Brigade, Yantai Shandong 264001, China)

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    摘要:

    针对现代导弹武器多约束、高精度制导的基本要求,在综合考虑带落角和末端攻角约束的条件下,用二次 型最优控制推导出一种新的最优末制导律。仿真结果表明,该末制导律既能够满足高精度制导的要求,同时也能 够满足对落角和末端攻角的控制要求。

    Abstract:

    In order to meet the requirements of the missile high-precision guilded. The considering the condi? tions under the constraints with the impact angle and the angle of attack, the new guidance law was deduced by the quadratic optimal control. The verified results showed that the guidance law with the impact angle and the angle of attack constraint was satisfied not only the requirements of high- precision guidance, but also the end of attack could be a good control.

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张友安,孙阳平,方悦,黄诘.带落角和末端攻角约束的最优末制导律[J].海军航空大学学报,2013,28(4):368-371
ZHANG You-an, SUN Yang-ping, FANG Yue, HUANG Jie. Optimal Guidance Law with Constrainton Terminal Impact Angle and Angle of Attack[J]. JOURNAL OF NAVAL AVIATION UNIVERSITY,2013,28(4):368-371

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  • 在线发布日期: 2016-07-07
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