Direction cosine matrix estimation from vector observations using a matrix kalman filter

D. Choukroun, H. Weiss, I. Y. Bar-Itzhackz, Y. Oshman

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

5 Scopus citations

Abstract

This work presents several estimation algorithms of the attitude matrix using vector observations. All the algorithms are state matrix Kalman filters that preserve the natural formulation of the attitude matrix statespace model equations. The filters feature an efficient, though simplified, estimation error covariance computation algorithm. Four different methods are proposed to enforce the orthogonality of the attitude matrix estimate. All the orthogonalization procedures accelerate the estimation convergence. The special case of unbiased gyros was considered when developing these filters. The performance of the different filters are demonstrated through extensive Monte-Carlo simulations. An augmented state matrix mathematical model is also developed, where the augmented state matrix includes the attitude matrix and a vector of constant gyro biases.

Original languageEnglish
Title of host publicationAIAA Guidance, Navigation, and Control Conference and Exhibit
StatePublished - 1 Dec 2003
Externally publishedYes
EventAIAA Guidance, Navigation, and Control Conference and Exhibit 2003 - Austin, TX, United States
Duration: 11 Aug 200314 Aug 2003

Publication series

NameAIAA Guidance, Navigation, and Control Conference and Exhibit

Conference

ConferenceAIAA Guidance, Navigation, and Control Conference and Exhibit 2003
Country/TerritoryUnited States
CityAustin, TX
Period11/08/0314/08/03

ASJC Scopus subject areas

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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