| 带落角和末端攻角约束的最优末制导律 |
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| 引用本文： | 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].海军航空工程学院学报,2013,28(4):368-371. |
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| 作者姓名： | 张友安 孙阳平 方悦 黄诘 |
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| 作者单位： | [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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| 基金项目： | 国家自然科学基金资助项目（61273058）;海军航空工程学院研究生创新基金资助项目 |
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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。
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| 关 键 词： | 落角约束 末端攻角约束 制导律 最优控制 |
| 收稿时间： | 2012/9/17 0:00:00 |
| 修稿时间： | 2013/1/14 0:00:00 |
Optimal Guidance Law with Constrainton Terminal Impact Angle and Angle of Attack |
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| ZHANG You-an,SUN Yang-ping,FANG Yue and HUANG Jie.Optimal Guidance Law with Constrainton Terminal Impact Angle and Angle of Attack[J].Journal of Naval Aeronautical Engineering Institute,2013,28(4):368-371. |
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| Authors: | ZHANG You-an SUN Yang-ping FANG Yue and HUANG Jie |
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| Institution: | (Naval Aeronautical and Astronautical University a. Department of Control Engineering; b. Graduate Students＇ Brigade, Yantai Shandong 264001, China) |
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| Abstract: | In order to meet the requirements of the missile high-precision guilded. The considering the conditions 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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| Keywords: | terminal impact angular constriaint constraint of terminal angle of attack guidance law optimal control |
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