Pilot-Involved-Oscillation Suppression Using Low-Order Antiwindup: Flight-Test Evaluation
Author:
Affiliation:
1. DLR, German Aerospace Center, 38108 Braunschweig, Germany
2. University of Leicester, Leicester, England LE1 7RH, United Kingdom
3. Universidad Nacional de Colombia, Colombia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.54441
Reference36 articles.
1. Pilot-Induced Oscillation Analysis and Prediction with Actuator Rate Limiting
2. Aircraft Handling Qualities and Pilot-Induced Oscillation Tendencies with Actuator Saturation
3. Investigating the Role of Rate Limiting in Pilot-Induced Oscillations
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