Studies on optimized algorithm for SINS under high dynamic

Zhao Fei Zhang, Jian Jun Luo, Bai Chun Gong

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

1 Scopus citations

Abstract

As to improve the attitude solving accuracy of strapdown inertial navigation system (SINS) boarded on the spacecraft for high dynamic application, a novel optimized coning error compensation algorithm is developed. Based on the rotation vector concept, a general scheme of N measurement samples coning error compensation by utilizing the last P measurement samples is proposed. Then, an optimized compensation algorithm is given in fixed frequency environment. And the key coefficients of this algorithm can be acquired by a simple matrix calculus rather than a complicated derivation. Finally, the algorithm is verified and tested by physical experiment. The results show that the coning error compensation accuracy does can be improved.

Original languageEnglish
Title of host publicationInformation Technology and Intelligent Transportation System - Volume 1, Proceedings of the International Conference on Information Technology and Intelligent Transportation Systems, ITITS 2015
EditorsLakhmi C. Jain, Xiangmo Zhao, Valentina Emilia Balas
PublisherSpringer Verlag
Pages67-75
Number of pages9
ISBN (Print)9783319387871
DOIs
StatePublished - 2017
EventInternational Conference on Information Technology and Intelligent Transportation Systems, ITITS 2015 - Xi’an, China
Duration: 12 Dec 201513 Dec 2015

Publication series

NameAdvances in Intelligent Systems and Computing
Volume454
ISSN (Print)2194-5357

Conference

ConferenceInternational Conference on Information Technology and Intelligent Transportation Systems, ITITS 2015
Country/TerritoryChina
CityXi’an
Period12/12/1513/12/15

Keywords

  • Coning error
  • Fixed frequency
  • Rotation vector
  • SINS

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