Thrust level used to optimize rocket trajectory depends on value of "switching function" K(t), and thrust can have intermediate value only where K(t) is zero; necessary conditions for drag-free intermediate-thrust subarc (in plane containing inverse-square-law central force field) are pursued to point of graphical representation; paper introduces graphical approach to analysis of planar intermediate-thrust ("singular") trajectories in inverse-square-law field; some analytical results are included.


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    Titel :

    Graphical analysis of singular trajectories for optimal navigation


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Gaston, C.A. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 9


    Erscheinungsdatum :

    1967


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Singular optimal atmospheric rocket trajectories

    KUMAR, RENJITH / KELLEY, HENRY J. | AIAA | 1988


    Optimal trajectories for space navigation

    Lawden, Derek F. | TIBKAT | 1963


    A graphical construct of time optimal trajectories

    ZAGALSKY, N. / IRONS, JR., R. / LINDQUIST, O. | AIAA | 1972