NASA NTRS · 20140008294
Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations
Abstract
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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Craun, Robert W., Acosta, Diana M., Beard, Steven D., Hardy, Gordon H., Leonard, Michael W., Weinstein, Michael. 2013-08-19. Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations. https://ntrs.nasa.gov/citations/20140008294
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