Formulations of general (inclined orbits and free end points) optimum 2-impulse orbital transfer problem lead to expressions that are analytically intractable; numerical techniques were developed and used to study optimum transfer modes; many orbit pairs yield 4 useful relative optima; parameter space was adopted to represent impulse function, i.e., impulse is function of takeoff point, arrival point, and transfer orbit semilatus rectum; as result, one may predict gross properties of "impulse function spaces" and determine optimum 2-impulse orbital transfer circumstances for any pair of elliptical orbits.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Optimum two-impulse orbital transfer and rendezvous between inclined elliptical orbits


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    McCue, G.A. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 8


    Erscheinungsdatum :

    1963


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :