Dynamic Testing of UAV Navigation System

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Date

2017-10

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Publisher

Kyiv, “Osvita Ukrainy”

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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Keywords

Navigation system, three-axis test table, unmanned aerial vehicle, dynamic test table system

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