Scheme developed handles general earth-orbit rendezvous mission combining functions of flight planning (targeting) and guidance into single, simple program for onboard computation; improvements have been made, including full-orbit phasing for close to minimum-propellant flight plans, as well as bielliptic-transfer trajectories for shorter flight times at generally higher cost, with chase and "lob" options providing further opportunity to trade fuel for time; targets can be changed in flight; complete rendezvous flight plans are computed in less than 1 sec; results from test cases show present capabilities.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Recent developments in variable point guidance for space rendezvous and rescue


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Schneider, A.M. (Autor:in) / Capen, E.B. (Autor:in) / Camiel, J.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Variable Deviated Pursuit for Rendezvous Guidance

    Ashwini Ratnoo | Online Contents | 2015



    Rendezvous guidance of space vehicles

    Tschauner, J. / Hempel, P. | Engineering Index Backfile | 1964