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惯性系统飞行试验精度检验方法
引用本文:肖正林,陈芳.惯性系统飞行试验精度检验方法[J].装备环境工程,2018,15(1):23-25.
作者姓名:肖正林  陈芳
作者单位:中国人民解放军96658部队,北京 100085,中国人民解放军96658部队,北京 100085
摘    要:目的针对传统工具误差分离方法得到的分离结果不够准确可信的问题,提出了一种利用等效误差实现对惯性系统精度判定的方法。方法首先基于主成分分析,定义等效误差,等效误差具有独立、无偏的性质。然后提出基于等效误差的假设检验判断惯性系统精度是否合格的方法。结果算例表明采用该方法可以实现惯性系统精度的可信判断。结论该方法解决了以往方法误差大,分析结论可信度不高的问题。

关 键 词:等效误差  主成分法  精度检验  惯性系统
收稿时间:2017/11/10 0:00:00
修稿时间:2018/1/15 0:00:00

A Method for Testing Accuracy of Inertial System in Flight Test
XIAO Zheng-lin and CHEN Fang.A Method for Testing Accuracy of Inertial System in Flight Test[J].Equipment Environmental Engineering,2018,15(1):23-25.
Authors:XIAO Zheng-lin and CHEN Fang
Institution:Troop 96658, PLA, Beijing 100085, China and Troop 96658, PLA, Beijing 100085, China
Abstract:Objective Aiming at the problem that results obtained by the traditional instrument error separation method are not accurate enough, a method for determining the accuracy of the inertial system by using equivalent error is proposed. Methods Firstly, the equivalent error which was independent and unbiased was defined based on the principal component analysis. Then, a method based on the hypothesis test of the equivalent error was put forward to determine the precision of the inertial system. Results The example showed that the method can be used to determine the inertial system accuracy credibly. Conclusion With this method, the problem that the error is large and the credibility is low in the previous approach is solved.
Keywords:equivalent error  principal component method  precision test  inertial system
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