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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Adaptive Orbit Determination for Interplanetary Spacecraft


    Contributors:

    Publication date :

    1996-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    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