A flight investigation of pilot-induced oscillation due to rate limiting

IEEE Aerospace Conference Proceedings

Volumn 3, Issue , 1998, Pages 59-74

  Mitchell, David G ^a   Kish, Brian A ^b   Seo, John S ^c  

^a Hoh Aeronautics Inc   (United States)

^b CaptUSAF ^*  (United States)

^c USAF   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AVIATORS; MILITARY AIRCRAFT; OSCILLATIONS;

AIRCRAFT DYNAMICS; FLIGHT TEST; HEAD UP DISPLAYS; PILOT-INDUCED OSCILLATIONS; RATE LIMIT; RATE LIMITING; US AIR FORCE;

AIRCRAFT DETECTION; FLIGHT DYNAMICS;

ACTUATOR RATE LIMITING; PILOT INDUCED OSCILLATIONS (PIO);

EID: 0031627703     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.1998.685777     Document Type: Conference Paper

References (20)

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3. David G. Mitchell and Roger H. Hoh, "Development of a Unified Method to Predict PIO, " AIAA Atmospheric Flight Mechanics Conference Proceedings, My 1996.
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9. George E. Cooper and Robert P. Harper Jr, Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities, NASA-TN-D-5153. April 1969.
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14. Department of Defense Interface Standard, Flying Qualities of Piloted Aircraft, MIL-STD-1797A, Revised-Notice 1, June 1995.
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