| 一种脉冲式空间拦截末端导引规律的设计 |
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| 引用本文： | 史小平,王子才.一种脉冲式空间拦截末端导引规律的设计[J].宇航学报,1996,17(1):29-34. |
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| 作者姓名： | 史小平 王子才 |
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| 作者单位： | 哈尔滨工业大学仿真中心 |
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| 摘 要： | 本文通过对空间拦截运动学模型的线性化处理，提出了一种脉冲式末端导引规律，它既满足脱靶量指标，又使轨控发动机的燃料最省，且易于工程实现。仿真结果表明该导引律性能良好
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| 关 键 词： | 脉冲式导引规律 空间拦截 最优控制 |
DESIGN OF AN IMPULSE TERMINAL GUIDANCE LAW OF SPACE INTERCEPTION |
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| Shi Xiaoping,Wang Zicai,Ke Qihong.DESIGN OF AN IMPULSE TERMINAL GUIDANCE LAW OF SPACE INTERCEPTION[J].Journal of Astronautics,1996,17(1):29-34. |
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| Authors: | Shi Xiaoping Wang Zicai Ke Qihong |
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| Abstract: | This paper provides an impulse terminal guidance law by linearizing the kinematical system of space interception under certain conditions. This guidance law not only satisfies the given missdistance index but also saves fuel of the trajectory-control-motor to the full extent. This guidance law is very easy to implement and is verified by numerical simulation. |
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| Keywords: | Impulse guidance law Space interception Optimal control |
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