This work introduces a dual accelerometer usage strategy for onboard space navigation. In the proposed algorithm the accelerometer is used to propagate the state when its value exceeds a threshold and it is used to estimate its errors otherwise. Numerical examples and comparison to other accelerometer usage schemes are presented to validate the proposed approach.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Dual Accelerometer Usage Strategy for Onboard Space Navigation


    Beteiligte:
    Zanetti, Renato (Autor:in) / D'Souza, Chris (Autor:in)

    Kongress:

    22nd AAS/AIAA Space Flight Mechanics Meeting ; 2012 ; Charleston, SC, United States


    Erscheinungsdatum :

    29.01.2012


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Dual Accelerometer Usage Strategy for Onboard Space Navigation

    Zanetti, Renato / D'Souza, Chris | AIAA | 2012



    Dual Accelerometer Usage Strategy for Onboard Space Navigation (AAS 12-198)

    Zanetti, R. / D Souza, C. / American Astronautical Society et al. | British Library Conference Proceedings | 2012