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:

    Publication date :

    2002


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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

    Hodel, A. S. / Shtessel, Yuri B. / Jackson, Scott | NTRS | 2002


    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