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Volumn , Issue , 2001, Pages 1512-1517

Computation of the zero error manifold for a problem of smooth vertical landing of an helicopter

Author keywords

Aerospace Systems; Non linear Oscillations; Output Regulation; Trajectory Tracking in Non linear Systems

Indexed keywords

CONTROL ENGINEERING;

EID: 84947474939     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.23919/ecc.2001.7076133     Document Type: Conference Paper
Times cited : (3)

References (6)
  • 3
    • 0031084757 scopus 로고    scopus 로고
    • Structurally stable output regulation of nonlinear systems
    • Byrnes C. I., Delli Priscoli F., Isidori A. & Kang W. (1997) Structurally stable output regulation of nonlinear systems. Automatica, 33(2), 369-385.
    • (1997) Automatica , vol.33 , Issue.2 , pp. 369-385
    • Byrnes, C.I.1    Delli Priscoli, F.2    Isidori, A.3    Kang, W.4
  • 4
    • 0032255577 scopus 로고    scopus 로고
    • Output tracking control design of a helicopter model based on approximate linearization
    • Tampa, Florida
    • Koo T. J. & Sastry S. (1998), Output Tracking Control Design of a Helicopter Model Based on Approximate Linearization, In Proc. of IEEE Conference on Decision and Control, Tampa, Florida.
    • (1998) Proc. of IEEE Conference on Decision and Control
    • Koo, T.J.1    Sastry, S.2
  • 6
    • 0002882474 scopus 로고
    • The construction of optimal linear and nonlinear regulators
    • A. Isidori and T. J Tarn editors. Birkhauser
    • Krener A., The Construction of Optimal Linear and Nonlinear Regulators. In Systems, Models and Feedback: Theory and Applications, A. Isidori and T. J Tarn editors. Birkhauser, 1992.
    • (1992) Systems, Models and Feedback: Theory and Applications
    • Krener, A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.