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:
    R. Zanetti (author) / C. D'Souza (author)

    Publication date :

    2012


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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

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