The results of the numerical tests performed in evaluating the interplanetary monitoring platform-16 orbit determination system are presented. The system is capable of performing orbit determination from satellite to satellite tracking data in applications technology satellite range and range rate format. The estimation scheme used is a Kalman filter, sequential (recursive) estimator. Descriptions of the tests performed and tabulations of the numerical results are included.


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    Title :

    Evaluation of the Imp-16 Microprocessor Orbit Determination System Filter


    Contributors:

    Publication date :

    1979


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English