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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    Title :

    Dual Accelerometer Usage Strategy for Onboard Space Navigation


    Contributors:

    Conference:

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


    Publication date :

    2012-01-29


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :



    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