Dynamic testing of UAV navigation system

V. Sineglazov, S. Dolgorukov
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引用次数: 1

Abstract

The paper considers dynamic test table system for navigation sensors testing and verification. The problem of test table confidence margin is considered taking into account different sources of errors. Estimation of frequency characteristics of sensors is shown by special test table criteria. The paper describes inertial navigation system experiment on dynamic test table in order to compensate navigation system parameters.
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无人机导航系统的动态测试
本文研究了动态试验台系统对导航传感器的测试与验证。在考虑不同误差来源的情况下,考虑了测试表置信裕度问题。对传感器的频率特性进行了估计,并给出了专用的试验台准则。为了补偿导航系统的参数,本文介绍了惯性导航系统在动态试验台上的实验。
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