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Volumn 16, Issue , 2005, Pages 1-6

Bifurcation analysis of flight control systems

Author keywords

Bifurcation; Departure; F 16; Flight control

Indexed keywords

BIFURCATION (MATHEMATICS); CONTROL SYSTEM ANALYSIS; DEGREES OF FREEDOM (MECHANICS); FREE FLIGHT; OBSERVABILITY; SUPERSONIC AIRCRAFT;

EID: 79960715376     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.3182/20050703-6-cz-1902.01961     Document Type: Conference Paper
Times cited : (9)

References (17)
  • 7
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    • Application of bifurcation theory to high angle of attack dynamics of the f-14 aircraft
    • Jahnke, C. C. and F. E. C. Culick (1994). Application of bifurcation theory to high angle of attack dynamics of the f-14 aircraft. Journal of Aircraft 31, 26-34.
    • (1994) Journal of Aircraft , vol.31 , pp. 26-34
    • Jahnke, C.C.1    Culick, F.E.C.2
  • 11
    • 0017007971 scopus 로고
    • On the flexibility offered by state feedback in multivariable systems beyond closed loop eigenvalue assignment
    • Moore, B. C. (1976). On the flexibility offered by state feedback in multivariable systems beyond closed loop eigenvalue assignment. IEEE Transactions on Automatic Control 21(5), 689-692.
    • (1976) IEEE Transactions on Automatic Control , vol.21 , Issue.5 , pp. 689-692
    • Moore, B.C.1
  • 12
    • 84881366001 scopus 로고    scopus 로고
    • Global nonlinear parametric modeling with application to f-16 aero- dynamics
    • Philadelphia
    • Morelli, Eugene A. (1998). Global nonlinear parametric modeling with application to f-16 aero- dynamics. In: American Control Conference. Philadelphia. pp. 997-1001.
    • (1998) American Control Conference , pp. 997-1001
    • Morelli, E.A.1
  • 14
    • 0003673079 scopus 로고    scopus 로고
    • Performance, stability, dynamics, and control of airplanes
    • AIAA, Reston
    • Pamadi, B. N. (1998). Performance, Stability, Dynamics, and Control of Airplanes. AIAA Education Series. AIAA. Reston.
    • (1998) AIAA Education Series
    • Pamadi, B.N.1
  • 15
    • 0020294670 scopus 로고
    • Flight control synthesis using robust output obsrvers
    • San Diego
    • Rynaski, E. G. (1982). Flight control synthesis using robust output obsrvers. In: AIAA Guidance and Control Conference. San Diego. pp. 825-831.
    • (1982) AIAA Guidance and Control Conference , pp. 825-831
    • Rynaski, E.G.1
  • 17
    • 8744278891 scopus 로고    scopus 로고
    • Nonlinear reconfiguration for asymmetric failures in a six degree-of-freedom f- 16
    • Boston
    • Thomas, S., H. G. Kwatny and B. C. Chang (2004). Nonlinear reconfiguration for asymmetric failures in a six degree-of-freedom f- 16. In: American Control Conference. Boston. pp. 1823-1829.
    • (2004) American Control Conference , pp. 1823-1829
    • Thomas, S.1    Kwatny, H.G.2    Chang, B.C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.