| 动基座惯导系统快速初始对准方案 |
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| 引用本文： | 杨海波,高广林,王瑞臣. 动基座惯导系统快速初始对准方案[J]. 导弹与航天运载技术, 2010, 0(5) |
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| 作者姓名： | 杨海波 高广林 王瑞臣 |
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| 作者单位： | 海军潜艇学院,青岛,266071;海军工程大学天津校区,天津,300450 |
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| 摘 要： | 由于动基座的非匀速运动,给惯导系统平台的调平带来了附加误差.通过分析动基座在水平方向的运动加速度,推出了惯导系统平台调平等效误差角模型,并给出了一种快速初始对准方案.
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| 关 键 词： | 动基座 惯导系统 初始对准 |
Inertial Navigation System Rapid Initial Alignment Concept on Moving Base |
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| Yang Haibo,Gao Guanglin,Wang Ruichen. Inertial Navigation System Rapid Initial Alignment Concept on Moving Base[J]. Missiles and Space Vehicles, 2010, 0(5) |
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| Authors: | Yang Haibo Gao Guanglin Wang Ruichen |
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| Affiliation: | Yang Haibo1,Gao Guanglin2,Wang Ruichen1(1.Navy Submarine Academy,Qingdao,266071,2.Tianjin Campus,Naval University of Engineering,Tianjin,300450) |
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| Abstract: | The unevenly movement of the moving base causes the additional error in adjustment of Inertial Navigation System(INS) platform.The horizontal acceleration of the moving base was analyzed in this article,and the model of equivalent error angle adjustment of INS was deduced.The concept that can realize Rapid Initial Alignment was brought forward. |
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| Keywords: | Moving base INS Initial Alignment |
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