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Transfer alignment in strapdown inertial navigation system using CCD star tracker

  • Chongmeng Zhang*
  • , Guochen Wang
  • *Corresponding author for this work
  • Tianjin Navigation Instrument Research Institute
  • Harbin Engineering University

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

Abstract

The devices error in inertial navigation system, especially gyro drift can mostly effect navigation precision, aim to make navigation system to work long time and with high precision of work, transfer alignment technology using Star tracker to estimate and compensate gyro drift and accelerometer bias is proposed with "velocity plus attitude" matching scheme, in which attitude information is provided by Star CCD star tracker and velocity information achieves from inertial navigation system, the simulation results indicates that gyro drift and acceleration bias can be fully estimated out in short time, whose precision can greatly improve by increasing estimation time.

Original languageEnglish
Title of host publication2011 IEEE International Conference on Signal Processing, Communications and Computing, ICSPCC 2011
DOIs
StatePublished - 2011
Externally publishedYes
Event2011 IEEE International Conference on Signal Processing, Communications and Computing, ICSPCC 2011 - Xi'an, China
Duration: 14 Sep 201116 Sep 2011

Publication series

Name2011 IEEE International Conference on Signal Processing, Communications and Computing, ICSPCC 2011

Conference

Conference2011 IEEE International Conference on Signal Processing, Communications and Computing, ICSPCC 2011
Country/TerritoryChina
CityXi'an
Period14/09/1116/09/11

Keywords

  • Integrated Navigation
  • Star tracker
  • Strapdown inertial navigation system
  • Transfer Alignment

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