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Volumn 2009, Issue , 2009, Pages

Highly efficient sigma point filter for spacecraft attitude and rate estimation

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHM FRAMEWORK; ANGULAR RATE; CLOSED FORM SOLUTIONS; NEW STRATEGY; NON-LINEARITY; NONLINEAR FILTERING ALGORITHM; NUMERICAL ACCURACY; RATE ESTIMATION; RATE ESTIMATOR; SIGMA POINT; SIGMA POINT FILTERS; SPACE MISSIONS; SPACECRAFT ATTITUDE; SPACECRAFT ATTITUDE DETERMINATION; UNSCENTED KALMAN FILTER;

EID: 75649142171     PISSN: 1024123X     EISSN: 15635147     Source Type: Journal    
DOI: 10.1155/2009/507370     Document Type: Article
Times cited : (21)

References (19)
  • 2
    • 21244437999 scopus 로고    scopus 로고
    • Unscented filtering and nonlinear estimation
    • Julier S. J., Uhlmann J. K., Unscented filtering and nonlinear estimation Proceedings of the IEEE 2004 92 3 401 422
    • (2004) Proceedings of the IEEE , vol.92 , Issue.3 , pp. 401-422
    • Julier, S.J.1    Uhlmann, J.K.2
  • 9
    • 0036058369 scopus 로고    scopus 로고
    • Reduced sigma point filters for the propagation of means and covariances through nonlinear transformations
    • May 2002 Anchorage, Alaska, USA
    • Julier S. J., Uhlmann J. K., Reduced sigma point filters for the propagation of means and covariances through nonlinear transformations 2 Proceedings of the American Control Conference (ACC 02) May 2002 Anchorage, Alaska, USA 887 892
    • Proceedings of the American Control Conference (ACC 02) , vol.2 , pp. 887-892
    • Julier, S.J.1    Uhlmann, J.K.2
  • 17
    • 0037352783 scopus 로고    scopus 로고
    • Attitude error representations for Kalman filtering
    • Markley F. L., Attitude error representations for Kalman filtering Journal of Guidance, Control, and Dynamics 2003 26 2 311 317
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.2 , pp. 311-317
    • Markley, F.L.1
  • 19
    • 85003406366 scopus 로고
    • Analytic steady-state accuracy solutions for two common spacecraft attitude estimators
    • Farrenkopf R. L., Analytic steady-state accuracy solutions for two common spacecraft attitude estimators Jounal of Guidance and Control 1978 1 4 282 284
    • (1978) Jounal of Guidance and Control , vol.1 , Issue.4 , pp. 282-284
    • Farrenkopf, R.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.