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Volumn , Issue , 2006, Pages 69-74

Modelling and control of a convertible VTOL aircraft

Author keywords

Aircraft control algorithm; Amplitude bounded input; Embbeded architecture; Nonlinear control; VTOL

Indexed keywords

MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; SYSTEM STABILITY; UNMANNED AERIAL VEHICLES (UAV);

EID: 39649102540     PISSN: 07431546     EISSN: 25762370     Source Type: Conference Proceeding    
DOI: 10.1109/cdc.2006.376915     Document Type: Conference Paper
Times cited : (31)

References (8)
  • 3
    • 39649120204 scopus 로고    scopus 로고
    • P. Castillo, R. Lozano A. Dzul, Modelling and control of mini flying machines, Springer-Verlag, July 2005.
    • P. Castillo, R. Lozano A. Dzul, "Modelling and control of mini flying machines, Springer-Verlag, July 2005.
  • 7
    • 39649104715 scopus 로고    scopus 로고
    • Aerodynamic Modelling of a Wing-in-Slipstream Tail-Sitter UAV
    • Williamsburg, Virginia, Nov. 5-7
    • H. Stone, "Aerodynamic Modelling of a Wing-in-Slipstream Tail-Sitter UAV", 2002 Biennial International Powered Lift Conference and Exhibit, Williamsburg, Virginia, Nov. 5-7,
    • (2002) Biennial International Powered Lift Conference and Exhibit
    • Stone, H.1
  • 8
    • 0028712602 scopus 로고    scopus 로고
    • Sussmann H, Sontag E and Yang Y. A General Result on the Stabilization of linear System Using Bounded Control IEEE TAC 1994 12 39 pp 2411-2425.
    • Sussmann H, Sontag E and Yang Y. "A General Result on the Stabilization of linear System Using Bounded Control" IEEE TAC 1994 vol (12) 39 pp 2411-2425.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.