The time-optimal slewing problem of flexible spacecraft is considered. The system is discretised by the assumed-modes method, and the problem is solved for a linearized model in reduced state space by parameter optimization. Optimality is verified by the maximal principle. The linear solution is used to obtain time-optimal solutions for the nonlinear problem.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Time optimal slewing of flexible spacecraft


    Weitere Titelangaben:

    Zeitoptimales Schwenken eines flexiblen Raumfahrzeugs


    Beteiligte:
    Ben-Asher, J. (Autor:in) / Burns, J.A. (Autor:in) / Cliff, E.M. (Autor:in)


    Erscheinungsdatum :

    1987


    Format / Umfang :

    5 Seiten, 11 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Time-optimal slewing of flexible spacecraft

    BEN-ASHER, JOSEPH / BURNS, JOHN A. / CLIFF, EUGENE M. | AIAA | 1992



    Planar, time-optimal, rest-to-rest slewing maneuvers of flexible spacecraft

    SINGH, GURKIRPAL / KABAMBA, PIERRE T. / MCCLAMROCH, N. HARRIS | AIAA | 1989


    Robust optimal control of flexible spacecraft during slewing maneuvers

    Ebrahimi, Asghar / Moosavian, S. Ali A. / Mirshams, Mehran | Tema Archiv | 2004