Traditional attitude control design of reusable launch vehicles involves independent design of autopilot and control allocation modules [SBB99], [SK97], [SHJ00], [PS00], [Hod00]. Unfortunately, this results in the potential for overly aggressive commands in the autopilot resulting in a loss of performance due to actuator saturation, particularly if the autopilot may suffer from integrator wind-up [HH01].


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    Titel :

    On-Line Computation of a Local Attainable Moment Set for Reusable Launch Vehicles


    Beteiligte:
    Hodel, A. S. (Autor:in) / Shtessel, Yuri B. (Autor:in) / Jackson, Scott (Autor:in)

    Kongress:

    2002 AIAA GN and C Conference ; 2002 ; Monterey, CA, United States


    Erscheinungsdatum :

    2002-01-09


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch





    AIAA-2002-4780 On-Line Computation of a Local Attainable Moment Set for Reusable Launch Vehicles

    Hodel, A. / Shtessel, Y. / AIAA | British Library Conference Proceedings | 2002


    Reusable launch vehicles

    Osmun, W.G. | Engineering Index Backfile | 1964


    Reusable launch vehicles

    DrDr Ruppe, H.O. | Elsevier | 1985