Title: The analysis of error control mechanism for single-axis rotation inertial navigation system
Abstract: It is significantly important to improve the performance of inertial navigation system navigation by controlling the negative effects on inertial navigation system for inertial measurement units.This paper analyses the error equations of the inertial navigation system,makes a focus on the inertial components accumulation effect on symmetrical position error,analyses the automatic constant error compensation mechanism of the inertial navigation system,and then discusses the error depressing of inertial components constant error,the scale factor error cased by rotating.Finally,the simulation for single-axis rotation mechanism validates the theory analysis.
Publication Year: 2012
Publication Date: 2012-01-01
Language: en
Type: article
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