| 平台单星复合制导方法研究 |
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| 作者姓名： | 张婕 王智 常晓华 洪蓓 |
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| 作者单位： | 北京宇航系统工程研究所,北京宇航系统工程研究所,北京宇航系统工程研究所,北京宇航系统工程研究所 |
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| 摘 要： | 为了提高武器命中精度,开展了平台单星复合制导方法研究。通过建立星敏感器观测量、平台失调角与落点偏差之间的联系,构建星光修正模型;同时利用数值寻优方法确定最佳星方位。仿真证实,平台单星制导方法能够有效降低制导工具误差,是提高导弹命中精度的有效手段。
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| 关 键 词： | 制导 最佳星 命中精度 |
Research on Inertial/Celestial Integrated Guidance System of Single Star |
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| Authors: | ZHANG Jie WANG Zhi CHANG Xiao-hua and Hong Bei |
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| Institution: | Beijing Institute of Astronautical Systems Engineering,Beijing Institute of Astronautical Systems Engineering,Beijing Institute of Astronautical Systems Engineering and Beijing Institute of Astronautical Systems Engineering |
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| Abstract: | In order to improve hit accuracy, inertial/celestial integrated guidance system of single star is researched. Through the establishment of the connection between the star sensor observables, platform disorders angle and impact point deviation, the celestial navigation correction model is built. Through numerical method on the orientation of the optimal single star is determined. Mathematical simulating results show that celestial navigation of single star can reduce guidance instrument error. It is an effective means to improve the hit accuracy. |
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