This paper presents an iterative method for three-axis magnetometer (TAM) calibration that makes use of three existing utilities recently incorporated into the attitude ground support system used at NASA's Goddard Space Flight Center. The method combines attitude-independent and attitude-dependent calibration algorithms with a new spinning spacecraft Kalman filter to solve for biases, scale factors, nonorthogonal corrections to the alignment, and the orthogonal sensor alignment. The method is particularly well-suited to spin-stabilized spacecraft, but may also be useful for three-axis stabilized missions given sufficient data to provide observability.


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    Titel :

    Iterative Magnetometer Calibration


    Beteiligte:
    Sedlak, Joseph (Autor:in)

    Kongress:

    AAS/AIAA Astrodynamics Specialists Conference ; 2006 ; Keystone, CO, United States


    Erscheinungsdatum :

    2006-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Iterative Magnetometer Calibration

    Sedlak, Joseph | AIAA | 2006


    Iterative Magnetometer Calibration AIAA Paper 2006-6386

    Sedlak, J. | British Library Conference Proceedings | 2006


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