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Volumn 11, Issue 4, 2005, Pages 543-560

Smart spring impedance control algorithm for helicopter blade harmonic vibration suppression

Author keywords

Active vibration suppression; Adaptive control; Individual blade control; Smart Spring

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; IMPULSE RESPONSE; SENSORS; TRANSFER FUNCTIONS; VIBRATIONS (MECHANICAL); WHITE NOISE; WIND TUNNELS;

EID: 17444421149     PISSN: 10775463     EISSN: None     Source Type: Journal    
DOI: 10.1177/1077546305052039     Document Type: Article
Times cited : (24)

References (15)
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  • 7
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    • Washington, DC
    • Millot, T. A. et al., 1998, "Flight test of active gear-mesh noise control on the S-76 aircraft," in American Helicopter Society 54th Annual Forum, Washington, DC.
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    • Millot, T.A.1
  • 8
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    • A control theory approach to the stability and transient analysis of the filtered-x LMS adaptive notch filter
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    • (1992) IEEE Transactions on Signal Processing , vol.40 , Issue.9 , pp. 2341-2346
    • Morgan, D.R.1    Sanford, C.2
  • 10
    • 17444372565 scopus 로고    scopus 로고
    • "Structural component having means for actively varying its stiffness to control vibrations," US patent 5,973,440
    • Nitzsche, F., Grewal, A., and Zimcik, D. G., 1999, "Structural component having means for actively varying its stiffness to control vibrations," US patent 5,973,440.
    • (1999)
    • Nitzsche, F.1    Grewal, A.2    Zimcik, D.G.3
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    • "Structural component having means for actively varying its stiffness to control vibrations," European Patent EP-996570-B1
    • Nitzsche, F., Grewal, A., and Zimcik, D. G., 2001, "Structural component having means for actively varying its stiffness to control vibrations," European Patent EP-996570-B1.
    • (2001)
    • Nitzsche, F.1    Grewal, A.2    Zimcik, D.G.3
  • 12
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    • Control laws for an active tunable vibration absorber designed for rotor blade damping augmentation
    • Nitzsche, F., Zimcik, D. G., Wickramashinghe, V., and Chen, Y., 2004, "Control laws for an active tunable vibration absorber designed for rotor blade damping augmentation," Aeronautical Journal 108(1), 35-42.
    • (2004) Aeronautical Journal , vol.108 , Issue.1 , pp. 35-42
    • Nitzsche, F.1    Zimcik, D.G.2    Wickramashinghe, V.3    Chen, Y.4
  • 13
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    • Development of a piezoelectric actuator for trailing edge flap control of full-scale rotor blades
    • Straub, F. K., Ngo, H. T., Anand, V., and Domzalski, D. B., 2001, "Development of a piezoelectric actuator for trailing edge flap control of full-scale rotor blades," Smart Materials and Structure 10(4), 25-34.
    • (2001) Smart Materials and Structure , vol.10 , Issue.4 , pp. 25-34
    • Straub, F.K.1    Ngo, H.T.2    Anand, V.3    Domzalski, D.B.4
  • 14
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    • Active isolation of multiple structural waves on a helicopter gearbox support strut
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    • (1997) Journal of Sound and Vibration , vol.205 , Issue.1 , pp. 81-101
    • Sutton, T.J.1    Elliott, S.J.2    Brennan, M.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.