To predict accurately free-flight motion of rocket near earth (or other oblate body) for trajectory design and guidance, gravitational effect of equatorial bulge must be accounted for; this can be done by solving equations of motion, based on gravitational potential model developed by J. P.Vinti; analysis is modified considerably to obtain solution suited to free-flight segments of ascent to satellite orbit, satellite de-orbit, ballistic missile, and spacecraft skip re-entry trajectories.


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    Titel :

    Vinti solution for free-flight rocket trajectories


    Weitere Titelangaben:

    AIAA J


    Beteiligte:

    Erschienen in:

    AIAA Journal ; 1 , n 6


    Erscheinungsdatum :

    1963


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    VINTI SOLUTION FOR FREE-FLIGHT ROCKET TRAJECTORIES

    TILLER, P. R. / WADSWORTH, D. V. | AIAA | 1963


    Vinti Solution for Free-Flight Rocket Trajectories

    DONALD VAN Z. WADSWORTH | AIAA | 1974


    Orbital Resonances in the Vinti Solution

    Zurita, Laura Duffy | British Library Conference Proceedings | 2017


    The Vinti Spheroidal Method for Satellite Orbits and Ballistic Trajectories

    Bonavito, Nino L. / Der, Gim J. / Vinti, John P. | AIAA | 1998


    Satellite Motion in a Vinti Potential

    Rater, L. M. / American Astronautical Society / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1996