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Volumn 8, Issue 6, 2000, Pages 883-894

Periodic control of helicopter rotors for attenuation of vibrations in forward flight

Author keywords

[No Author keywords available]

Indexed keywords

FORWARD FLIGHT; LINEAR TIME PERIODIC SYSTEM; PERIODIC CONTROL; VIBRATION ATTENUATION;

EID: 0034315289     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.880590     Document Type: Article
Times cited : (92)

References (20)
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  • 4
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    • McKillip, R.1
  • 5
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    • Periodic model-following controller for the independent modal control of individual blades using smart structures
    • Cernobbio, Italy
    • F. Nitsche, "Periodic model-following controller for the independent modal control of individual blades using smart structures," in Proc. 19th Europ. Rotorcraft Forum, Cernobbio, Italy, 1993.
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    • Nitsche, F.1
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    • On the zero dynamics of helicopter rotor loads
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  • 9
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    • Princeton, NJ: Princeton Univ. Press
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    • Johnson, W.1
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    • Active control of vibrations in helicopters via pole assignment techniques
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    • Bittanti, S.1    Moiraghi, L.2
  • 12
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    • Modeling helicopter rotor dynamics with ADAMS
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    • V. Bertogalli, F. Bisi, and M. Lovera, "Modeling helicopter rotor dynamics with ADAMS," in 1995 ADAMS User Conf., Ann Arbor, MI, 1995, pp. 291-311.
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  • 15
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  • 18
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.