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Space relative navigation filter based on-board radar observation

  • Ma Weihua*
  • , Luo Jianjun
  • , Wang Mingming
  • , Yang Bo
  • *Corresponding author for this work
  • Northwestern Polytechnical University Xian

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

Abstract

The absolute attitude error of chaser vehicle is always neglected in observation equation of space relative navigation filter when chaser satellite on-board radar using as the measurement sensor. But the attitude error could affect relative navigation filter precision in fact. The new observation equation, which contains the absolute attitude error of chaser vehicle, is constructed. And the plan, using equivalent measurement error as attitude error, is put forward. The simulations show that the filter precision of relative position and velocity descend when attitude error is big, and the precision is improved when attitude equivalent error is introduced to filter. The plan of attitude equivalent error is proved to be feasible.

Original languageEnglish
Title of host publicationProceedings of the 2009 2nd International Congress on Image and Signal Processing, CISP'09
DOIs
StatePublished - 2009
Externally publishedYes
Event2009 2nd International Congress on Image and Signal Processing, CISP'09 - Tianjin, China
Duration: 17 Oct 200919 Oct 2009

Publication series

NameProceedings of the 2009 2nd International Congress on Image and Signal Processing, CISP'09

Conference

Conference2009 2nd International Congress on Image and Signal Processing, CISP'09
Country/TerritoryChina
CityTianjin
Period17/10/0919/10/09

Keywords

  • Attitude error
  • Chaser satellite
  • Equivalent measurement error
  • On-board radar
  • Space relative navigation filter

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