| 导弹在真空段自由飞行时捷联惯导系统脉冲数据辨识 |
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| 引用本文： | 熊玮 刘石泉. 导弹在真空段自由飞行时捷联惯导系统脉冲数据辨识[J]. 战术导弹技术, 1993, 0(1): 46-51 |
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| 作者姓名： | 熊玮 刘石泉 |
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| 作者单位： | 066基地设计所，066基地设计所 |
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| 摘 要： | 介绍了导弹在真空段自由飞行时加速度计的误差模型及其输出脉冲数据的选取与处理。重点探讨脉冲数据的识方法,并通过具体实例说明了该方法的有效性及其应用价值。
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| 关 键 词： | 地对地导弹 健联式惯性导航 加速度计 误差分析 辨识 |
IDENTIFICATION OF PULSE DATA OF STRAPDOWN INERTIAL NAVIGATION SYSTEM IN VACCUM FREE-FLIGHT PHASE OF MISSILE |
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| Xiong Wei Liu Shiquan Research Institute of Base of MAS. IDENTIFICATION OF PULSE DATA OF STRAPDOWN INERTIAL NAVIGATION SYSTEM IN VACCUM FREE-FLIGHT PHASE OF MISSILE[J]. Tactical Missile Technology, 1993, 0(1): 46-51 |
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| Authors: | Xiong Wei Liu Shiquan Research Institute of Base of MAS |
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| Affiliation: | Xiong Wei Liu Shiquan Research Institute of 066 Base of MAS |
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| Abstract: | Being in vaccum free-flight phase, The error model of the acceierometer and the selection and precessing of its output puise data are intrc-luccd. The identification method of puse data is probed emphapcais The effectiveness and application value of this identification method are expiaincd by example. |
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| Keywords: | Ground to ground missile Strpdown inertial navigation Accelerometer Error anaivsis Identificanon |
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