Analysis of error suppression performance in the carrier angle motion status for rotation for FOG inertial navigation system

Hairong Wang*, Zhihong Deng, Bo Wang

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Citations (Scopus)

Abstract

Rotation modulation is an effective method of reducing the errors of inertial navigation system (INS). However, when the carrier is in angular motion status, especially when the heading angle changes in wide range, the performance of error suppression will be influenced. In this paper, according to the error rotation modulation principle, based on attitude error equation of rotation inertial navigation system, the mechanism that the modulation effect is influence by angular motion of carrier is analyzed. The coupling impact from the variation of carrier angle and rotation angular velocity of IMU on error rotation modulation effect is investigated. The simulation test show the result that the errors suppression performance is influenced by the variation of amplitude and rotation angle rate. And it is confirmed that low rotary rate can improve accuracy of the rotary navigation system in angular motion status of carrier.

Original languageEnglish
Title of host publicationProceedings of the 33rd Chinese Control Conference, CCC 2014
EditorsShengyuan Xu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages1026-1030
Number of pages5
ISBN (Electronic)9789881563842
DOIs
Publication statusPublished - 11 Sept 2014
EventProceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, China
Duration: 28 Jul 201430 Jul 2014

Publication series

NameProceedings of the 33rd Chinese Control Conference, CCC 2014
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

ConferenceProceedings of the 33rd Chinese Control Conference, CCC 2014
Country/TerritoryChina
CityNanjing
Period28/07/1430/07/14

Keywords

  • carrier angle motion
  • error suppression performance
  • inertial measurement unit
  • rotary inertial navigation system

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