The interplanetary orbit problem has been traditionally solved using least-squares techniques. Due to operational limitations of this method, a Kalman filter approach has been proposed for future missions which includes all spacecraft and measurement modeling states in the filter.


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    Titel :

    Adaptive Orbit Determination for Interplanetary Spacecraft


    Beteiligte:

    Erscheinungsdatum :

    01.01.1996


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Adaptive Orbit Determination for Interplanetary Spacecraft

    Burkhart, P.D. | Online Contents | 1996


    Adaptive orbit determination for interplanetary spacecraft

    Burkhart, P. D. / Bishop, Robert H. | AIAA | 1996


    Adaptive Orbit Determination for Interplanetary Spacecraft

    Burkhart, P. D. / Bishop, R. H. / American Astronautical Society et al. | British Library Conference Proceedings | 1996



    Adaptive Orbit Determination for Interplanetary Spacecraft

    Bishop, Robert H. / Burkhart, P. Daniel | NTRS | 1995