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Volumn 37, Issue 10, 2003, Pages 1277-1295

Modélisation et commande non linéaire pour un hélicoptere birotor coaxial

Author keywords

Backstepping techniques; Direct lyapunov method; Helicopter dynamics; Nonlinear control

Indexed keywords


EID: 70349408200     PISSN: 12696935     EISSN: None     Source Type: Journal    
DOI: 10.3166/jesa.37.1277-1295     Document Type: Article
Times cited : (2)

References (14)
  • 4
    • 84883072839 scopus 로고    scopus 로고
    • Output tracking control design of a helicopter model based on approximate linearization
    • Tampa, Florida, États-Unis 16-18 décembre
    • Koo J., Sastry S.,« Output Tracking Control Design of a Helicopter Model Based on Approximate Linearization », Actes du congrés : 37th Conference on Decision and Control, Tampa, Florida, États-Unis, 16-18 décembrel998.
    • (1998) Actes du Congrés : 37th Conference on Decision and Control
    • Koo, J.1    Sastry, S.2
  • 6
    • 85038731144 scopus 로고    scopus 로고
    • Hover Control Using Lyapunov Control Function Design for an Autonomous Model Helicopter
    • novcmbrel999, Hcudiasyc URM 6599, Université de Technologic de Compicgne
    • Mahony R., Hamel T.,« Hover Control Using Lyapunov Control Function Design for an Autonomous Model Helicopter », rapport technique no 99/221, novcmbrel999, Hcudiasyc URM 6599, Université de Technologic de Compicgne.
    • Rapport Technique No 99/221
    • Mahony, R.1    Hamel, T.2
  • 7
    • 0033332942 scopus 로고    scopus 로고
    • Hover control via Lyapunov control for an autonomous model helicopter
    • Phoenix, Arizona, États-Unis, de q́cmbrel999
    • Mahony R., Hamel T., Dzul A., « Hover control via Lyapunov control for an autonomous model helicopter », Actes du congrés : 38th Conference on Decision and Control, Phoenix, Arizona, États-Unis, de q́cmbrel999, p. 3490-3495.
    • Actes du Congrés : 38th Conference on Decision and Control , pp. 3490-3495
    • Mahony, R.1    Hamel, T.2    Dzul, A.3
  • 9
    • 0029204637 scopus 로고
    • Control of Rotor Speed for a Model Helicopter : AAAAAA Design Cycle
    • Seattle, Washington, États-Unis, 21-23 juin
    • Nieuwstadt M. V., Morris J. C,« Control of Rotor Speed for a Model Helicopter : a Design Cycle », Actes du congrés : American Control Conference ACC'95, Seattle, Washington, États-Unis, 21-23 juin l995, p. 688-692.
    • (1995) Actes du Congrés : American Control Conference ACC'95 , pp. 688-692
    • Nieuwstadt, M.V.1    Morris, J.C.2
  • 10
    • 0032163450 scopus 로고    scopus 로고
    • Real time trajectory generation for differentially flat systems
    • John Wiley & Sons, Ltd
    • Nieuwstadt M. V., murray R., « Real time trajectory generation for differentially flat systems », International Journal of Robust and Nonlinear Control, vol.8, no 11, 1997, p. 995-1020, John Wiley & Sons, Ltd.
    • (1997) International Journal of Robust and Nonlinear Control , vol.8 , Issue.11 , pp. 995-1020
    • Nieuwstadt, M.V.1    Murray, R.2
  • 11
    • 77950084015 scopus 로고
    • Helicopter performance, stability and control
    • Prouty R. W., Helicopter performance, stability and control, Krieger Pub. Co., 1990.
    • (1990) Krieger Pub. Co.
    • Prouty, R.W.1
  • 14
    • 84930608290 scopus 로고    scopus 로고
    • On the regulation of a helicopter system: A trajectory planning approach for the liouvillian model
    • Karlsruhe, Germany, 31 aout- 03 septembre
    • Sira-Ramirez H., Castro-Linares R., « On the regulation of a helicopter system: a trajectory planning approach for the Liouvillian Model », Actes du congrés : European Control Conference ECC'99, Karlsruhe, Germany, 31 aout- 03 septembrel999.
    • (1999) Actes du Congrés : European Control Conference ECC'99
    • Sira-Ramirez, H.1    Castro-Linares, R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.