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Volumn 2005, Issue , 2005, Pages

Wing-flaperon and swashplate control for whirl-flutter stability augmentation of a soft-inplane tiltrotor

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; CONTROL SYSTEMS; DAMPING; FEEDBACK; FLUTTER (AERODYNAMICS); ROBUSTNESS (CONTROL SYSTEMS); ROTORS; STABILITY; SYSTEM STABILITY;

EID: 33746595792     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (20)
  • 2
    • 4143088193 scopus 로고
    • Wind tunnel tests of a full scale hingeless prop/rotor designed for the boeing model 222 tilt rotor aircraft
    • Boeing Vertol Co., Oct.
    • Magee, J. P. and Alexander, H. R., "Wind Tunnel Tests of a Full Scale Hingeless Prop/Rotor Designed for the Boeing Model 222 Tilt Rotor Aircraft," NASA CR 114664, Boeing Vertol Co., Oct. 1973.
    • (1973) NASA CR 114664
    • Magee, J.P.1    Alexander, H.R.2
  • 4
    • 0017465566 scopus 로고
    • Optimal control alleviation of tilting proprotor gust response
    • March
    • Johnson, W., "Optimal Control Alleviation of Tilting Proprotor Gust Response," Journal of Aircraft, vol. 14, no. 3, March 1977, pp. 301-308.
    • (1977) Journal of Aircraft , vol.14 , Issue.3 , pp. 301-308
    • Johnson, W.1
  • 5
    • 0005868146 scopus 로고
    • Tilt-rotor flutter control in cruise flight
    • December
    • Nasu, K.-i., "Tilt-Rotor Flutter Control in Cruise Flight," NASA TM 88315, December, 1986.
    • (1986) NASA TM 88315
    • Nasu, K.-I.1
  • 6
    • 0025723339 scopus 로고
    • Alleviation of whirl-flutter on tilt-rotor aircraft using active controls
    • Phoenix, AZ, May 6-8
    • van Aken, J. M., "Alleviation of Whirl-Flutter on Tilt-Rotor Aircraft Using Active Controls," Proceedings of the 47th Annual AHS Forum, Phoenix, AZ, May 6-8, 1991.
    • (1991) Proceedings of the 47th Annual AHS Forum
    • Van Aken, J.M.1
  • 12
    • 3042637007 scopus 로고    scopus 로고
    • Exploratory studies in generalized predictive control for active aeroelastic control of tiltrotor aircraft
    • Kvaternik, R. G., "Exploratory Studies in Generalized Predictive Control for Active Aeroelastic Control of Tiltrotor Aircraft," NASA TM-2000-210552.
    • NASA TM-2000-210552
    • Kvaternik, R.G.1
  • 13
    • 4143067951 scopus 로고    scopus 로고
    • Tiltrotor whirl flutter alleviation using actively controlled wing flaperons
    • Baltimore, Maryland, June 7-10
    • Hathaway, E., and Gandhi, F., "Tiltrotor Whirl Flutter Alleviation Using Actively Controlled Wing Flaperons," Presented at the AHS International 60th Annual Forum and Technology Display, Baltimore, Maryland, June 7-10, 2004.
    • (2004) AHS International 60th Annual Forum and Technology Display
    • Hathaway, E.1    Gandhi, F.2
  • 15
    • 0030671882 scopus 로고    scopus 로고
    • Tiltrotor vibration reduction through higher harmonic control
    • Virginia Beach, Virginia, April 29- May 1
    • Nixon, M. W., Kvaternik, R. G., and Settle, T. B., "Tiltrotor Vibration Reduction Through Higher Harmonic Control," Proceedings of the 53rd Annual AHS Forum, Virginia Beach, Virginia, April 29- May 1, 1997.
    • (1997) Proceedings of the 53rd Annual AHS Forum
    • Nixon, M.W.1    Kvaternik, R.G.2    Settle, T.B.3
  • 16
    • 0041765120 scopus 로고    scopus 로고
    • Modeling refinements in simple tiltrotor whirl flutter analyses
    • July
    • Hathaway, E. L. and Gandhi, F., "Modeling Refinements in Simple Tiltrotor Whirl Flutter Analyses," Journal of the American Helicopter Society, vol. 48, no. 3, July 2003, pp. 186-198.
    • (2003) Journal of the American Helicopter Society , vol.48 , Issue.3 , pp. 186-198
    • Hathaway, E.L.1    Gandhi, F.2
  • 18
    • 4143136430 scopus 로고    scopus 로고
    • Design optimization for improved tiltrotor whirl flutter stability
    • Friedrichshafen, Germany, 16-18 September
    • Hathaway, E. and Gandhi, F., "Design Optimization for Improved Tiltrotor Whirl Flutter Stability," Proceedings of the 29th European Rotorcraft Forum, Friedrichshafen, Germany, 16-18 September 2003.
    • (2003) Proceedings of the 29th European Rotorcraft Forum
    • Hathaway, E.1    Gandhi, F.2
  • 19
    • 0032119906 scopus 로고    scopus 로고
    • Optimized aeroelastic couplings for alleviation of helicopter ground resonance
    • July-August
    • Gandhi, F., and Hathaway, E., "Optimized Aeroelastic Couplings for Alleviation of Helicopter Ground Resonance," Journal of Aircraft, Vol. 35, No. 4, July-August 1998, pp. 582-590.
    • (1998) Journal of Aircraft , vol.35 , Issue.4 , pp. 582-590
    • Gandhi, F.1    Hathaway, E.2
  • 20
    • 0035079263 scopus 로고    scopus 로고
    • Concurrent optimization of aeroelastic couplings and rotor stiffness for the alleviation of helicopter aeromechanical instability
    • Jan.-Feb.
    • Hathaway, E., and Gandhi, F., "Concurrent Optimization of Aeroelastic Couplings and Rotor Stiffness for the Alleviation of Helicopter Aeromechanical Instability," Journal of Aircraft, Vol. 38, No. 1, Jan.-Feb. 2001, pp. 69-80.
    • (2001) Journal of Aircraft , vol.38 , Issue.1 , pp. 69-80
    • Hathaway, E.1    Gandhi, F.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.