Analysis of earth orbit rendezvous in terms of maneuver geometry served as basis for establishing requirements for visually sensed rendezvous guidance information; analysis of physical environment supported evaluation of sensory basis; visual capabilities were examined in terms of sensitivity, cross range motion perception, range, and range rate determinations; estimates of sensitivity and variability are presented where available; conclusions are drawn regarding adequacy of available data, and are given for future areas of study. (11037)


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    Titel :

    Visual sensing of spacecraft guidance information -- Earth orbit rendezvous maneuvers


    Weitere Titelangaben:

    NASA CR


    Beteiligte:
    Seidenstein, S. (Autor:in) / Kincaid, Jr., W.K. (Autor:in) / Kreezer, G.L. (Autor:in) / Utter, D.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    245 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Visual Sensing of Spacecraft Guidance Information. Earth Orbit Rendezvous Maneuvers

    W. K. Kincaid / G. L. Kreezer / S. Seidenstein et al. | NTIS | 1968



    Visual sensing of spacecraft guidance information. Earth orbit rendezvous maneuvers

    Kincaid, W. K., Jr. / Kreezer, G. L. / Seidenstein, S. et al. | NTRS | 1968


    Lyapunov-based Spacecraft Rendezvous Maneuvers using Differential Drag

    Perez, David / Bevilacqua, Riccardo | AIAA | 2011


    Lyapunov-based Spacecraft Rendezvous Maneuvers using Differential Drag

    Perez, D. / Bevilacqua, R. / American Institute of Aeronautics and Astronautics; Confederation of European Aerospace Societies | British Library Conference Proceedings | 2011