An Adaptive Stick-Gain to Reduce Pilot-Induced Oscillation Tendencies

• 1 March 1982
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
• Vol. 5  (2) , 138-142
• https://doi.org/10.2514/3.56150

Abstract

Keywords

• ADAPTIVE STICK
• PILOT INDUCED
• OSCILLATION TENDENCIES
• REDUCE PILOT
• STICK GAIN
• INDUCED OSCILLATION