Flight-Test Evaluation of an Adaptive Controller for Flying Qualities Specification and Protection
Author:
Affiliation:
1. Barron Associates, Inc., Charlottesville, Virginia 22901
2. Systems Technology, Inc., Hawthorne, California 90250
3. NASA Armstrong Flight Research Center, Edwards, California 93523
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.G000873
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4. Recommended Practices for Exposing Pilot-Induced Oscillations or Tendencies in the Development Process
5. Evolution of the honeywell first-generation adaptive autopilot and its applications to F-94, F-101, X-15, and X-20 vehicles.
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1. Stability limit of human-in-the-loop model reference adaptive control architectures;International Journal of Control;2017-07-04
2. Vehicle Upset Detection and Recovery for Onboard Guidance and Control;Journal of Guidance, Control, and Dynamics;2017-04
3. Development and Pilot-In-The-Loop Evaluation of Robust Upset-Recovery Guidance;AIAA Guidance, Navigation, and Control Conference;2016-01-01
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