GPS/惯导组合定位方案及试验数据分析

doi:10.3969/j.issn.1009-086x.2018.01.011

现代防御技术 ›› 2018, Vol. 46 ›› Issue (1): 69-73.DOI: 10.3969/j.issn.1009-086x.2018.01.011

GPS/惯导组合定位方案及试验数据分析

魏鹏涛¹, 王艳²

1.火箭军指挥学院,湖北武汉 430012;
2.渭南技师学院,陕西渭南 714000

收稿日期:2016-12-25 修回日期:2017-06-09 出版日期:2018-02-28 发布日期:2020-11-25
作者简介:魏鹏涛(1983-),男,陕西白水人。讲师,博士,主要研究方向为大地测量。通信地址:430012 湖北武汉江岸区二七路145号战术教研室 E-mail:weipengtao09@163.com

GPS/INS Combined Positioning Scheme and Its Experimental Data Analysis

WEI Peng-tao¹, WANG Yan²

1. The Rocket Force Command College,Hubei Wuhan 430012,China;
2. Weinan Technician College,Shaanxi Weinan 714000,China

Received:2016-12-25 Revised:2017-06-09 Online:2018-02-28 Published:2020-11-25

摘要/Abstract

摘要： 导弹机动发射阵地的快速定位是提升其机动发射能力的关键问题。针对目前快速定位采用的“GPS实时动态测量”方案和“惯性测量”方案,分析其优缺点,并在此基础上提出了组合定位方案,通过实验证明了该方案的可行性。

关键词: GPS/惯导, 导弹机动发射, 快速定位, 组合方案, 试验分析, 卡尔曼滤波, 定位误差, 应用趋势

Abstract: The rapid positioning of the missile’s mobile launch position is the key problem to improve its maneuverability. Based on the schemes of GPS real time dynamic measurement and inertia measurement as adopted by the missile's mobile launch positioning, the predominance and shortcoming are analyzed. A new combined positioning scheme is put forward and its feasibility is proved through experiment.

Key words: GPS(global positioning system)/INS(inertial navigation system), missile mobile launching, quick positioning, compound scheme, test analysis, Kalman filtering, position error, application trend

中图分类号:

TJ768
P228.4

魏鹏涛, 王艳. GPS/惯导组合定位方案及试验数据分析[J]. 现代防御技术, 2018, 46(1): 69-73.

WEI Peng-tao, WANG Yan. GPS/INS Combined Positioning Scheme and Its Experimental Data Analysis[J]. Modern Defense Technology, 2018, 46(1): 69-73.

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GPS/惯导组合定位方案及试验数据分析

GPS/INS Combined Positioning Scheme and Its Experimental Data Analysis

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