Identifying the pilot in pilot-induced oscillations
Author:
Affiliation:
1. Hoh Aeronautics, Inc., Lomita, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3985
Reference19 articles.
1. A Limited Flight Test Investigation of Pilot-Induced Oscillation Due to Elevator Rate Limiting (HAVE LIMITS)
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1. Transport Aircraft Certification Testing for Pilot Closed Loop Dynamic Instability;2018 Flight Testing Conference;2018-06-24
2. Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings – A design perspective;Progress in Aerospace Sciences;2015-07
3. Adverse rotorcraft pilot couplings—Past, present and future challenges;Progress in Aerospace Sciences;2013-10
4. Identifying a PIO Signature - New Techniques Applied to an Old Problem;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2006-06-25
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