Baseline guidance and navigation strategy for an ecliptic projection of the Encke flyby mission consider solar electric propulsion stage parameters in generating optimized and targeted trajectory control. Results show the Encke relative approach error to be dominated by ephemerical uncertainties, particularly the velocity components.


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    Title :

    System design impact of guidance and navigation analysis for a SEPS 1979 Encke flyby


    Contributors:
    Hong, P. (author)


    Publication date :

    1975-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :



    Encke flyby science package

    NEWBURN, R. / WEDDELL, J. | AIAA | 1973



    Comet Encke Flyby Asteroid Rendezvous Mission

    ALAN L. FRIEDLANDER | AIAA | 1974


    Terminal navigation analysis for the 1980 comet Encke slow flyby mission

    JACOBSON, R. / MCDANELL, J. / RINKER, G. | AIAA | 1973