| 比例导引导弹理想弹道的动态修正 |
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| 引用本文： | 孙凯斌.比例导引导弹理想弹道的动态修正[J].沈阳航空工业学院学报,1997,14(1):11-21. |
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| 作者姓名： | 孙凯斌 |
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| 作者单位： | 航天部长虹制造公司 |
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| 摘 要： | 本文基于近红外导弹比例导引的要求，研讨了比例导引规律的实现问题，提出了比例导引理想弹道及其线性化，并实际考虑导弹在发射时的瞄准误差和在制导过程中目标机动运动，进行动态修正的基础上，得出了指导正确设计和使用比例引导弹的重要结论。
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| 关 键 词： | 比例导引 线性化 动态修正 导弹弹道 理想弹道 |
Dynamic Correction for the Ideal Trajectory of the Proportional Guidance Missiles |
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| Sun Kaibin.Dynamic Correction for the Ideal Trajectory of the Proportional Guidance Missiles[J].Journal of Shenyang Institute of Aeronautical Engineering,1997,14(1):11-21. |
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| Authors: | Sun Kaibin |
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| Abstract: | Based on the requirement of the near - infrared missiles' proportional guidance, realizingthe proportional guidance was discussed in this article. And the proportional guidance idealtrajectory and its linearization were also given out here. on the basis of considering .the aim-ing error in practical launching missiles, and thinking over the dynamic correction of thetarget's maneuvering movement in the course of guidance, the important conclusion aboutguiding the correct designing and using proportional guidance missiles were given out in thearticle |
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| Keywords: | proportional guidance linearization dynamic correction |
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