Handling qualities degradation in tilt-rotor aircraft following flight control system failures

30th European Rotorcraft Forum

Volumn 2005, Issue , 2005, Pages 661-675

  Cameron, Nell ^a   Padfield, Gareth D ^a  

^a UNIVERSITY OF LIVERPOOL   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

CIVIL AIRCRAFTS; CIVIL TILT ROTORS; FLIGHT SAFETY; TOLERABLE ACTUATION RATES;

ACTUATORS; AIRCRAFT ACCIDENTS; FLIGHT DYNAMICS; HELICOPTER ROTORS; MATHEMATICAL MODELS; WINGS;

CONTROL SYSTEM ANALYSIS;

EID: 33745577964     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Nannoni, F.; Giancamilli, G.; Cicale, M.,"ERICA: The European Advanced Tilt Rotor", proceedings of the European Rotorcraft Forum, Moscow, 2001
2. st
3. th February 2002
4. Cooper, G. E.; Harper, Jr. R. P. - "The Use of Pilot Rating in The Evaluation of Aircraft Handling Qualities" - NASA Technical Note, TN D-5153, National Aeronautics and Space Administration, Washington D. C. -April 1969
5. Manimala, B., et. al. - Load Alleviation in Tilt Rotor Aircraft Through Active Control; Modelling and Controlling Concepts, Royal Aeronautical Journal, vol 108 no 1082, April 2004, pp 169-184
6. Padfield, G.D., White, M.D., Flight Simulation in Academia; HELIFLIGHT in its first year of operation, The Aeronautical Journal of the Royal Aeronautical Society, Sept, 2003
7. th American Helicopter Society Annual Forum, Montreal, June 2002 (accepted for publication in the J. American Helicopter Society).
8. th European Rotorcraft Forum, Friedrichshafen, Germany, Sept 2003
9. Padfield, G. D., "Criteria For Civil Tilt Rotor Handling Qualities in Conversion Mode", RHILP/UoL/TRO5/1.0 D4, May 2002
10. N. N. Military Standard, - Flying Qualities of Piloted Aircraft, MIL-STD-1797A, Department of Defense, 30 January 1990