Problem considered is that of finding perturbation solutions of differential equations of motion of vehicle moving under constant low-thrust acceleration; vehicle is initially moving in circular Kepler orbit; second-order perturbation theory is derived for vehicle departing from circular orbit; trajectory is produced by thrust vector maintained at constant, but arbitrarily chosen, angle with respect to radius vector; graphical results of second-order theory are presented which show representative low-thrust trajectories.


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    Titel :

    Perturbation solutions for low-thrust rocket trajectories


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Johnson, D.P. (Autor:in) / Stumpf, L.W. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 10


    Erscheinungsdatum :

    1965


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :