Micro-rendezvous operation is defined as phase of orbital rendezvous which starts at relative range on order of 50-100,000 ft and terminates in docking operation; display of navigation data in forms of control criteria, which involve specification of thrust and vehicle attitude requirements, is introduced; control criteria requiring minimum of predisplay computation and resulting in simple cockpit displays are developed for orthogonal thrust vectors system, single vectored thrust system, and on-off system.


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    Titel :

    Control criteria for manual orbital rendezvous


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Beteiligte:
    Born, D.C. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    25 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Orbital rendezvous simulator

    Levin, E. / Ward, J. | Engineering Index Backfile | 1959


    Manned Control of Orbital Rendezvous

    E. Levin / J. Ward | NTIS | 1959


    Orbital rendezvous techniques

    MONDA ERIC W / KUTTER BERNARD F | Europäisches Patentamt | 2022

    Freier Zugriff

    Orbital rendezvous techniques

    Dowlen, E.M. / Seddon, J. | Engineering Index Backfile | 1964


    Automated orbital rendezvous considerations

    Lea, R.N. | Tema Archiv | 1988