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.


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    Titel :

    Dual Accelerometer Usage Strategy for Onboard Space Navigation


    Beteiligte:
    R. Zanetti (Autor:in) / C. D'Souza (Autor:in)

    Erscheinungsdatum :

    2012


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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