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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    Title :

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


    Contributors:

    Conference:

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


    Publication date :

    2002-01-09


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English





    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