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Volumn 216, Issue 6, 2002, Pages 477-496

Dynamic modelling and open-loop control of a twin rotor multi-input multi-output system

Author keywords

Helicopter; Open loop control; System identification; Twin rotor MIMO system; Vibration suppression

Indexed keywords

CONTROL SYSTEMS; DEGREES OF FREEDOM (MECHANICS); FEEDBACK CONTROL; LOW PASS FILTERS; RESONANCE; VIBRATION CONTROL;

EID: 0036964195     PISSN: 09596518     EISSN: None     Source Type: Journal    
DOI: 10.1243/095965102321042236     Document Type: Conference Paper
Times cited : (47)

References (21)
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  • 3
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  • 8
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    • System identification methods for aircraft flight control development and validation
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    • Tischler, M. B. System identification methods for aircraft flight control development and validation. In Advances in Aircraft Flight Control (Ed. M. B. Tischler), 1996, pp. 35-69 (Taylor and Francis, London).
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    • Tischler, M.B.1
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    • Modelling and control of a twin rotor multi-input multi-output system
    • Chicago, Illinois, June
    • Ahmad, S. M., Chipperfield, A. J. and Tokhi, M. O. Modelling and control of a twin rotor multi-input multi-output system. In Proceedings of the American Control Conference, Chicago, Illinois, June 2000, pp. 1720-1724.
    • (2000) Proceedings of the American Control Conference , pp. 1720-1724
    • Ahmad, S.M.1    Chipperfield, A.J.2    Tokhi, M.O.3
  • 12
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    • Parametric modelling and dynamic characterization of a two-degree-of-freedom twin rotor multi-input multi-ouput system
    • Ahmad, S. M., Chipperfield, A. J. and Tokhi, M. O. Parametric modelling and dynamic characterization of a two-degree-of-freedom twin rotor multi-input multi-ouput system. Proc. Instn Mech. Engrs, Part G, Journal of Aerospace Engineering, 2001, 215(G2), 63-78.
    • (2001) Proc. Instn Mech. Engrs, Part G, Journal of Aerospace Engineering , vol.215 , Issue.G2 , pp. 63-78
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  • 13
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  • 14
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.