A mathematical model is reported for determination of satellite position, velocity, and attitude using landmark coordinates as observables. This model, although developed with respect to earth stabilized missions, Tiros-N and Nimbus-G in particular, is applicable to any earth stabilized satellite in general.


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    Titel :

    Utilization of landmark data in attitude/orbit determination


    Beteiligte:
    Siddalingaiah, H. (Autor:in) / Desai, P. S. (Autor:in)


    Erscheinungsdatum :

    1975-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Orbit and attitude state recoveries from Landmark data

    Fuchs, A. F. / Velez, C. E. / Goad, C. C. | NTRS | 1975


    Orbit and attitude state recoveries from Landmark data

    Fuchs, A. F. / Velez, C. E. / Goad, C. C. | NTRS | 1975


    Autonomous landmark tracking orbit determination strategy

    Miller, J. K. / Cheng, Y. | NTRS | 2003


    Autonomous landmark tracking orbit determination strategy

    Miller, J. K. / Cheng, Y. | NTRS | 2003


    Autonomous Landmark Tracking Orbit Determination Strategy (AAS 03-614)

    Miller, J. K. / Cheng, Y. / American Astronautical Society | British Library Conference Proceedings | 2004