In order to advance research in the area of pilot induced oscillations, a reliable method to create PIOs in a simulated environment is necessary. Using a boundary avoidance tracking task, researchers performing an evaluation of control systems were able to create PIO events in 42% of cases using a nominal aircraft, and 91% of cases using an aircraft with reduced actuator rate limits. The simulator evaluation took place in the NASA Ames Vertical Motion Simulator, a high-fidelity motion-based simulation facility.


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    Title :

    Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations


    Contributors:
    R. W. Craun (author) / D. M. Acosta (author) / S. D. Beard (author) / G. H. Hardy (author) / M. W. Leonard (author) / M. Weinstein (author)

    Publication date :

    2013


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations

    Craun, Robert / Acosta, Diana M. / Beard, Steven D. et al. | AIAA | 2013


    Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations

    Craun, Robert W. / Acosta, Diana M. / Beard, Steven D. et al. | NTRS | 2013


    Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations (AIAA 2013-4688)

    Craun, R. / Acosta, D.M. / Beard, S.D. et al. | British Library Conference Proceedings | 2013