Automatic terminal guidance logic for rendezvous of 2 space vehicles in orbit, treating specifically phase between terminal acquisition and final docking; system, termed attenuated intercept, initiates intercept orbit, softened by dilating time to intercept; characteristics of system were evaluated by computer simulations for noncoplanar elliptic relative orbits; ability of system to accommodate range of thrust levels is shown; multiple start nonthrottleable engines appear adequate for task.


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    Titel :

    Attenuated intercept satellite rendezvous system


    Weitere Titelangaben:

    ARS J


    Beteiligte:
    Shapiro, M. (Autor:in)

    Erschienen in:

    ARS Journal ; 31 , n 12


    Erscheinungsdatum :

    1961


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Optimal impulsive intercept with low-thrust rendezvous return

    Lembeck, Catherine A. / Prussing, John E. | NTRS | 1993



    Optimal impulsive intercept with low-thrust rendezvous return

    LEMBECK, CATHERINE A. / PRUSSING, JOHN E. | AIAA | 1993