메뉴 건너뛰기




Volumn 39, Issue 3, 2003, Pages 1103-1112

Two-parameter bifurcation analysis of longitudinal flight dynamics

Author keywords

[No Author keywords available]

Indexed keywords

BIFURCATION (MATHEMATICS); COMPUTER SIMULATION; FIGHTER AIRCRAFT; MANEUVERABILITY; MATHEMATICAL MODELS; NONLINEAR SYSTEMS; OSCILLATIONS;

EID: 0344272282     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2003.1238764     Document Type: Letter
Times cited : (13)

References (11)
  • 2
    • 84997796772 scopus 로고
    • High angle-of-attack dynamic behavior of a model high performance fighter aircraft
    • AIAA Paper 88-4368, Aug. 1988
    • Planeaux, J. B., and Barth, T. J. (1988). High angle-of-attack dynamic behavior of a model high performance fighter aircraft. AIAA Paper 88-4368, Aug. 1988.
    • (1988)
    • Planeaux, J.B.1    Barth, T.J.2
  • 3
    • 84997447799 scopus 로고
    • Bifurcation analysis of a model fighter aircraft with control augmentation
    • AIAA Paper 90-2836, Aug. 1990
    • Planeaux, J. B., Beck, J. A., and Baumann, D. D. (1990) Bifurcation analysis of a model fighter aircraft with control augmentation. AIAA Paper 90-2836, Aug. 1990.
    • (1990)
    • Planeaux, J.B.1    Beck, J.A.2    Baumann, D.D.3
  • 4
    • 0031189150 scopus 로고    scopus 로고
    • Bifurcation analysis of a highly augmented aircraft model
    • Avanzini, G., and de Matteis, G. (1997) Bifurcation analysis of a highly augmented aircraft model. Journal of Guidance, Control, and Dynamics, 20, 4 (1997), 754-759.
    • (1997) Journal of Guidance, Control, and Dynamics , vol.20 , Issue.4 , pp. 754-759
    • Avanzini, G.1    De Matteis, G.2
  • 5
    • 0032164995 scopus 로고    scopus 로고
    • Bifurcation analysis of eigenstructure assignment control in a simple nonlinear aircraft model
    • Gibson, L. P., Nichols, N. K., and Litteboy, D. M. (1998) Bifurcation analysis of eigenstructure assignment control in a simple nonlinear aircraft model. Journal of Guidance, Control, and Dynamics, 21, 5 (1998), 792-798.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.5 , pp. 792-798
    • Gibson, L.P.1    Nichols, N.K.2    Litteboy, D.M.3
  • 6
    • 0028195691 scopus 로고
    • Application of bifurcation theory to the high angle-of-attack dynamics of the F-14
    • Jahnke, C. C., and Culick, F. E. C. (1994) Application of bifurcation theory to the high angle-of-attack dynamics of the F-14. Journal of Aircraft, 31, 1 (1994), 26-34.
    • (1994) Journal of Aircraft , vol.31 , Issue.1 , pp. 26-34
    • Jahnke, C.C.1    Culick, F.E.C.2
  • 9
    • 0034825750 scopus 로고    scopus 로고
    • Analysis of longitudinal flight dynamics: A bifurcation-theoretic approach
    • Liaw, D.-C., and Song, C-C. (2001) Analysis of longitudinal flight dynamics: A bifurcation-theoretic approach. Journal of Guidance, Control, and Dynamics, 24, 1 (2001), 109-116.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.1 , pp. 109-116
    • Liaw, D.-C.1    Song, C.-C.2
  • 10
    • 0017537095 scopus 로고
    • Design of nonlinear automatic flight control systems
    • (1977)
    • Garrard, W. L., and Jordan, J. M. (1977) Design of nonlinear automatic flight control systems. Automatica, 13, 5 (1977), 497-505.
    • (1977) Automatica , vol.13 , Issue.5 , pp. 497-505
    • Garrard, W.L.1    Jordan, J.M.2
  • 11
    • 0038250060 scopus 로고
    • Computer Science Dept., Concordia University, Jan. 1986
    • Doedel, E. J. (1986) AUTO 86 User Manual Computer Science Dept., Concordia University, Jan. 1986.
    • (1986) AUTO 86 User Manual
    • Doedel, E.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.