Kalman filtering techniques are combined with a semianalytical orbit generator to develop a sequential orbit determination algorithm. The algorithm is investigated for computational efficiency, accuracy, and radius of convergence by comparison with truth ephemerides and a Cowell special perturbations filters (GTDS). Test cases relevant to satellite navigation are examined.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Semiannalytical satellite theory and sequential estimation


    Contributors:


    Publication date :

    1980-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Staring-imaging satellite pointing estimation based on sequential ISAR images

    WANG, Canyu / JIANG, Libing / ZHONG, Weijun et al. | Elsevier | 2024

    Free access

    NAVSTAR/GPS satellite selection for sequential receivers

    Noe, P. S. / Parsiani, H. | NTRS | 1979



    Sequential Design of Satellite Formations with Invariant Distances

    Ning, Yu / Avendano, Martin E. / Mortari, Daniele | AIAA | 2011