The following paper is presented in viewgraph format and topics include: (1) exact solutions are difficult to obtain for higher order systems; (2) impulsive forces cannot be implemented directly; (3) exact solution provide the basis for judging the optimality of approximate techniques; and (4) properties of the exact solution can be used to develop improved approximations. Furthermore, the author discusses a floating harmonic oscillator whose model possesses rigid and flexible body motion characteristics of the proposed spacecraft.


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    Titel :

    Fuel Optimal Propulsive Reboost of Flexible Spacecraft


    Beteiligte:
    J. Redmond (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Fuel optimal propulsive reboost of flexible spacecraft

    SILVERBERG, LARRY / REDMOND, JIM | AIAA | 1992


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    Silverberg, L. | Online Contents | 1993



    Fuel-optimal propulsive reboost of flexible spacecraft

    SILVERBERG, LARRY / REDMOND, JIM | AIAA | 1993


    Fuel-optimal propulsive reboost of flexible spacecraft

    Silverberg, Larry / Redmond, Jim | NTRS | 1993