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Volumn 2, Issue , 2008, Pages 1127-1137

Active pitch link actuator for impedance control of helicopter vibration

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE NOISE CONTROL; ACTUATORS; APL (PROGRAMMING LANGUAGE); CONTROL SYSTEM ANALYSIS; CONTROL THEORY; FLIGHT CONTROL SYSTEMS; HELICOPTERS; LATTICE VIBRATIONS; PROJECT MANAGEMENT; STIFFNESS; TESTING; VIBRATIONS (MECHANICAL);

EID: 50049128380     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (14)

References (14)
  • 1
    • 10044235772 scopus 로고    scopus 로고
    • Straub, Friedrich K.; Kennedy, Dennis K.; Stemple, Alan D.; Anand, V. R.; Birchette, Terry S., Development and whirl tower test of the SMART active flap rotor, Smart Structures and Materials 2004: Industrial and Commercial Applications of Smart Structures Technologies. Edited by Anderson, Eric H. Proceedings of the SPIE, 5388, pp. 202-212 (2004). (SPIE Homepage), July 2004.
    • Straub, Friedrich K.; Kennedy, Dennis K.; Stemple, Alan D.; Anand, V. R.; Birchette, Terry S., "Development and whirl tower test of the SMART active flap rotor", Smart Structures and Materials 2004: Industrial and Commercial Applications of Smart Structures Technologies. Edited by Anderson, Eric H. Proceedings of the SPIE, Volume 5388, pp. 202-212 (2004). (SPIE Homepage), July 2004.
  • 3
  • 4
    • 0031682889 scopus 로고    scopus 로고
    • th Annual Forum of the American Helicopter Society, May 20-22 1998, Washington, DC, USA, v 1, 1998, p 378-390, 1998.
    • th Annual Forum of the American Helicopter Society, May 20-22 1998, Washington, DC, USA, v 1, 1998, p 378-390, 1998.
  • 6
    • 34547584234 scopus 로고    scopus 로고
    • Active rotor control by flaps for vibration reduction - full scale demonstrator and first flight test results
    • 12-14 Sep, NLR, Maastricht, the Netherlands
    • Roth, D., Enenkl, B., Dietrich, O., "Active rotor control by flaps for vibration reduction - full scale demonstrator and first flight test results", 32nd European Rotorcraft Forum, 12-14 Sep 2006, NLR, Maastricht, the Netherlands, Vol. 1, pp 801-814, 2007.
    • (2006) 32nd European Rotorcraft Forum , vol.1 , pp. 801-814
    • Roth, D.1    Enenkl, B.2    Dietrich, O.3
  • 7
    • 0035250528 scopus 로고    scopus 로고
    • Optimal control of helicopter vibration through cyclic variations in the blade root stiffness
    • Anusonti-Intra, P. and Ghandi, F., "Optimal control of helicopter vibration through cyclic variations in the blade root stiffness," Smart Materials and Structures, Vol. 10, 2001, pp. 86-95.
    • (2001) Smart Materials and Structures , vol.10 , pp. 86-95
    • Anusonti-Intra, P.1    Ghandi, F.2
  • 8
    • 50249131192 scopus 로고    scopus 로고
    • Daniel Feszty, Fred Nitzsche, Kostyantyn Khomutov, Brian K. Lynch, Andrei Mander, F. Démet Ülker, Design and instrumentation of the SHARCS scaled rotor with three independent control systems, Paper no. 080166, 64th Annual Forum of the American Helicopter Society, 29 April -1 May 2008, Montreal, QC, Canada, 2008.
    • Daniel Feszty, Fred Nitzsche, Kostyantyn Khomutov, Brian K. Lynch, Andrei Mander, F. Démet Ülker, "Design and instrumentation of the SHARCS scaled rotor with three independent control systems", Paper no. 080166, 64th Annual Forum of the American Helicopter Society, 29 April -1 May 2008, Montreal, QC, Canada, 2008.
  • 9
    • 50049084649 scopus 로고    scopus 로고
    • Semi-active control systems based on blade root and pitch link variable stiffness smart-spring and trailing edge flap to reduce aeroelastic vibratory loads at the hub of helicopters
    • Thesis of Laurea
    • Knollseiden, M. and Rossini, L., Semi-active control systems based on blade root and pitch link variable stiffness smart-spring and trailing edge flap to reduce aeroelastic vibratory loads at the hub of helicopters," University of Rome "Tre" College of Engineering, Thesis of "Laurea", 2004.
    • (2004) University of Rome Tre
    • Knollseiden, M.1    Rossini, L.2
  • 10
    • 0343559156 scopus 로고
    • Can Smart Materials Modify Blade Root Boundary Conditions to Attenuate Helicopter Vibration?
    • E. Breitbach, B.K. Wada and M. Natori, Editors, Technomic, Lancaster, PA
    • Nitzsche, F., Lammering, R. and Breitbach, E., "Can Smart Materials Modify Blade Root Boundary Conditions to Attenuate Helicopter Vibration?", 4th International Conference on Adaptive Structures, Cologne, Germany, November 2-4, 1993, E. Breitbach, B.K. Wada and M. Natori, Editors, Technomic, Lancaster, PA, 1994, pp. 139-150.
    • (1993) 4th International Conference on Adaptive Structures, Cologne, Germany, November 2-4 , pp. 139-150
    • Nitzsche, F.1    Lammering, R.2    Breitbach, E.3
  • 13
    • 23144467649 scopus 로고    scopus 로고
    • Acoustic Validation of a New Code Using Particle Wake Aerodynamics and Geometrically-Exact Beam Structural Dynamics
    • Opoku, D.G., Nitzsche, F., "Acoustic Validation of a New Code Using Particle Wake Aerodynamics and Geometrically-Exact Beam Structural Dynamics", Aeronautical Journal, Vol 109, pp. 257-267, 2005.
    • (2005) Aeronautical Journal , vol.109 , pp. 257-267
    • Opoku, D.G.1    Nitzsche, F.2
  • 14
    • 1242306809 scopus 로고    scopus 로고
    • Control laws for an active tunable vibration absorber designed for aeroelastic damping augmentation
    • F. Nitzsche, D. Zimcik, V. Wickramasinghe and C. Yong, "Control laws for an active tunable vibration absorber designed for aeroelastic damping augmentation," The Aeronautical Journal, Vol. 108, No. 1079, 2004, pp. 35-42.
    • (2004) The Aeronautical Journal , vol.108 , Issue.1079 , pp. 35-42
    • Nitzsche, F.1    Zimcik, D.2    Wickramasinghe, V.3    Yong, C.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.