| 一种适用于攻击地面固定目标的最优再入机动制导律 |
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| 引用本文： | 陈克俊,赵汉元.一种适用于攻击地面固定目标的最优再入机动制导律[J].宇航学报,1994,15(1):1-7. |
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| 作者姓名： | 陈克俊 赵汉元 |
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| 作者单位： | 国防科技大学 |
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| 摘 要： | 本文运用飞行力学原理和现代控制理论，对攻击地面固定目标的飞行器的再入机动制导方法进行了研究。在考虑飞行器命中目标时有落地速度和速度角要求的条件下，推导出了一种适用于攻击地面固定目标的最优再入机动导引律。并通过模拟计算分析论证了该制导规律的正确性。
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| 关 键 词： | 制导 再入机动 最优导引规律 |
AN OPTIMAL REENTRY MANEUVER GUIDANCE LAW APPLYING TO ATTACK THE GROUND FIXED TARGET |
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| Chen Kejun,Zhao Hanyuan.AN OPTIMAL REENTRY MANEUVER GUIDANCE LAW APPLYING TO ATTACK THE GROUND FIXED TARGET[J].Journal of Astronautics,1994,15(1):1-7. |
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| Authors: | Chen Kejun Zhao Hanyuan |
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| Institution: | National University of Defense Technology |
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| Abstract: | In this paper,the method of reentry maneuver guidance applying to attack the ground fixed target is described by using flight dynamics principle and modern control theory.Under the condition that the vehicle requires velocity and velocity path angle falling to the ground as hitting the target,the law is derived,an optimal reentry maneuver guidance law applying to attack the ground fixed target.and the it's correctness is proved by means of analog computation. |
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| Keywords: | guidance reentry maneuver optimal steering law |
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