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    Title :

    Finite-thrust explicit guidance law for nearly circular orbital rendezvous.


    Author / Creator :

    ZEE, C.-H. /GRUMMAN AIRCRAFT ENGINEERING CORP., GUIDANCE AND CONTROLSECTION, TRAJECTORY ANALYSIS GRO


    Contributors:
    ZEE, C.-H. (author)

    Published in:

    Publication date :

    1967




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Optimal guidance approximation for quasi-circular orbital rendezvous

    Kelley, H.J. / Dunn, J.C. | Engineering Index Backfile | 1964



    Optimal low-thrust orbital rendezvous

    MARINESCU, A. | AIAA | 1976