| 空空导弹捷联惯导系统总体设计与仿真研究 |
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| 引用本文： | 鲁浩,位晓峰. 空空导弹捷联惯导系统总体设计与仿真研究[J]. 电光与控制, 2007, 14(2): 128-132 |
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| 作者姓名： | 鲁浩 位晓峰 |
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| 作者单位： | 北京航空航天大学,北京,100083;中国空空导弹研究院,河南,洛阳,471009;中国空空导弹研究院,河南,洛阳,471009 |
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| 摘 要： | 探讨了空空导弹捷联惯导系统的总体设计技术,指出了系统设计时应考虑的几个主要问题,从总体设计的角度对捷联惯导系统的性能仿真环境和算法进行了分析和研究,并建立了系统仿真的模型框图,在此基础上进行了系统仿真和算法优化.
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| 关 键 词： | 空空导弹 捷联惯导 总体设计 数学仿真 |
| 文章编号： | 1671-637X（2007）02-0128-05 |
| 修稿时间： | 2005-12-192006-02-20 |
Simulation research and overall design for SINS of air-to-air missile |
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| LU Hao,WEI Xiao-feng. Simulation research and overall design for SINS of air-to-air missile[J]. Electronics Optics & Control, 2007, 14(2): 128-132 |
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| Authors: | LU Hao WEI Xiao-feng |
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| Affiliation: | 1. Beijing University of Aeronautics Astronautics, Beijing 100083, China ; 2. China Airborne Missile Academy, Luoyang 471009, China |
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| Abstract: | We discussed the overall design of Strapped-down Inertial Navigation System(SINS) of air-to-air missile,and indicated some problems that should be considered in design of the system.From the view of overall design,we analyzed the environments of performance simulation and the algorithmic models for SINS,and established the block diagram for system simulation. On which basis we also carried out system simulation and algorithm optimization. |
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| Keywords: | air - to - air missile SINS overall design simulation |
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