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Volumn 11, Issue 7, 2003, Pages 781-795

Multivariable control of the longitudinal and lateral dynamics of a fly-by-wire helicopter

Author keywords

Flight control; Flight test; H infinity control; Handling qualities; Helicopters

Indexed keywords

BANDWIDTH; CONTROL EQUIPMENT; CONTROL SYSTEM ANALYSIS; HELICOPTERS; OPTIMIZATION;

EID: 0041302137     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(02)00189-2     Document Type: Article
Times cited : (40)

References (27)
  • 1
    • 0042494904 scopus 로고    scopus 로고
    • Aeronautical design standard performance specification. Handling qualities requirements for military rotorcraft. ADS-33E-PRF
    • Anonymous. Redstone Arsenal, Alabama
    • Anonymous. (2000). Aeronautical Design Standard Performance Specification. Handling qualities requirements for military rotorcraft. ADS-33E-PRF. US Army Aviation and Missile Command. Aviation Engineering Directorate. Redstone Arsenal, Alabama.
    • (2000) US Army Aviation and Missile Command. Aviation Engineering Directorate
  • 10
    • 0032050814 scopus 로고    scopus 로고
    • An empirical correction for improving off-axes response in flight-mechanics helicopter models
    • Mansur, M. H., & Tischler, M. B. (1998). An empirical correction for improving off-axes response in flight-mechanics helicopter models. Journal of the American Helicopter Society, 43(2), 94-102.
    • (1998) Journal of the American Helicopter Society , vol.43 , Issue.2 , pp. 94-102
    • Mansur, M.H.1    Tischler, M.B.2
  • 15
    • 0019681684 scopus 로고
    • Theoretical prediction of dynamic inflow derivatives
    • Pitt, D. M., & Peters, D. A. (1981). Theoretical prediction of dynamic inflow derivatives. Vertica, 5(1), 21-34.
    • (1981) Vertica , vol.5 , Issue.1 , pp. 21-34
    • Pitt, D.M.1    Peters, D.A.2
  • 19
    • 0042494903 scopus 로고
    • The national aeronautical establishment airborne simulator facility
    • Sattler, D. E. (1984). The national aeronautical establishment airborne simulator facility. NRC, NAE Misc, 58.
    • (1984) NRC, NAE Misc , vol.58
    • Sattler, D.E.1
  • 22
    • 0041994069 scopus 로고    scopus 로고
    • Configuration of the DERA HELISIM model to represent the flight dynamics of the NRC Bell 205 fly-by-wire research helicopter
    • Strange, M. E., & Howitt, J. (1997). Configuration of the DERA HELISIM model to represent the flight dynamics of the NRC Bell 205 fly-by-wire research helicopter. DERA Technical report ASI FMCITR97459/1.
    • (1997) DERA Technical Report ASI FMCITR97459/1
    • Strange, M.E.1    Howitt, J.2
  • 24
    • 0031332814 scopus 로고    scopus 로고
    • Gain scheduled flight control via 2 degree-of-freedom H-infinity optimization
    • Walker, D. J. (1997). Gain scheduled flight control via 2 degree-of-freedom H-infinity optimization. Proceedings of the Institute of Mechanical Engineers, 211(Part I), 263-268.
    • (1997) Proceedings of the Institute of Mechanical Engineers , vol.211 , Issue.PART 1 , pp. 263-268
    • Walker, D.J.1
  • 25
  • 26
    • 0030105228 scopus 로고    scopus 로고
    • Advanced helicopter flight control using two-degree-of-freedom H∞ optimization
    • Walker, D. J., & Postlethwaite, I. (1996). Advanced helicopter flight control using two-degree-of-freedom H∞ optimization. Journal of Guidance, Control, and Dynamics, 19(2), 461-468.
    • (1996) Journal of Guidance, Control, and Dynamics , vol.19 , Issue.2 , pp. 461-468
    • Walker, D.J.1    Postlethwaite, I.2
  • 27
    • 0024881414 scopus 로고
    • H-infinity design and the improvement of helicopter handling qualities
    • Yuc, A., Postlethwaite, I., & Padfield, G. D. (1989). H-infinity design and the improvement of helicopter handling qualities. Vertica, 13(2), 119-132.
    • (1989) Vertica , vol.13 , Issue.2 , pp. 119-132
    • Yuc, A.1    Postlethwaite, I.2    Padfield, G.D.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.