Several minimum-fuel, aerodynamically controlled, orbital plane change problems are formulated and solved as optimal control problems. A gradient projection algorithm is used to iteratively modify both the control functions, angle of attack and bank angle, and two control parameters to obtain the optimal trajectory. The atmospheric flight profile is combined with two Keplerian (two-body vacuum flight) arcs so that a complete orbit-to-orbit analysis results. The vehicle used in this investigation is the Space Transportation System Shuttle Orbiter. The effects of heat load constraint level and plane change angle are analysed.


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    Titel :

    Minimum-fuel aerodynamic orbital plane change maneuvers


    Beteiligte:
    Joosten, B. K. (Autor:in) / Pierson, B. L. (Autor:in)

    Kongress:

    Aerospace Sciences Meeting ; 1981 ; St. Louis, MO


    Erscheinungsdatum :

    01.01.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Minimum-fuel aerodynamic orbital plane change maneuvers

    JOOSTEN, B. / PIERSON, B. | AIAA | 1981


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    Minimum-Time Orbital Phasing Maneuvers

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