| 基于机载捷联惯导计算导弹初始姿态的算法 |
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| 引用本文： | 陈宇,付书堂,刘建团. 基于机载捷联惯导计算导弹初始姿态的算法[J]. 航空兵器, 2016, 0(2): 29-31. DOI: 10.19297/j.cnki.41-1228/tj.2016.02.005 |
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| 作者姓名： | 陈宇 付书堂 刘建团 |
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| 作者单位： | 1. 中国空空导弹研究院,河南洛阳,471009;2. 陆军航空局驻洛阳地区军事代表室,河南洛阳,471009 |
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| 摘 要： | 随着惯导技术的发展,机载主惯导逐渐用捷联惯导替代平台式惯导,由此带来了火控系统计算导弹姿态算法的变化。本文研究了惯性导航系统算法,总结出基于机载捷联主惯导的导弹姿态算法。通过仿真验证,该算法计算精度满足要求,可以用于空空导弹导航系统初始化。
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| 关 键 词： | 空空导弹 捷联惯导 初始校准 导弹姿态 算法设计 |
Initial Attitude Algorithm of Missile Based on Airborne SINS |
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| Abstract: | With the development of inertial navigation technology, airborne platform inertial naviga-tion system is substituted gradually by SINS, which causes the change of missile attitude algorithm calcu-lated by fire control system.Research on the inertial navigation system algorithm is done and the attitude algorithm base on airborne SINS is summarized.The calculation accuracy of the algorithm meets the re-quirement and it can be used in the initialization of air-to-air missile navigation system. |
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| Keywords: | air-to-air missile SINS initial alignment missile attitude algorithm design |
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