-
1
-
-
0020178857
-
Bifurcation analysis of nonlinear aircraft dynamics
-
J. V. Carroll and R. K. Mehra. Bifurcation analysis of nonlinear aircraft dynamics. J. Guidance, 5: 5, 529-536, 1982.
-
(1982)
J. Guidance
, vol.5
, Issue.5
, pp. 529-536
-
-
Carroll, J.V.1
Mehra, R.K.2
-
4
-
-
0028195691
-
Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14
-
C. C. Jahnke and F. E. C. Culick. Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14. J. Aircraft, 31: 26-34, 1994.
-
(1994)
J. Aircraft
, vol.31
, pp. 26-34
-
-
Jahnke, C.C.1
Culick, F.E.C.2
-
6
-
-
84983197016
-
Departure analysis of a twin-finned, high performance combat. aircraft
-
USA, AIAA-96-3369-CP, American Institute of Aeronautics and Astronautics
-
Y. Patel and P. R. Smith. Departure analysis of a twin-finned, high performance combat. aircraft. In AIAA Atmospheric Flight Mechanics Conference Technical Papers, pages 80-87, USA, 1996. AIAA-96-3369-CP, American Institute of Aeronautics and Astronautics.
-
(1996)
AIAA Atmospheric Flight Mechanics Conference Technical Papers
, pp. 80-87
-
-
Patel, Y.1
Smith, P.R.2
-
7
-
-
0031220604
-
Application of bifurcation methods to nonlinear flight dynamics problems
-
M. G. Goman, G. I. Zagainov, and A. V. Khramtsovsky. Application of bifurcation methods to nonlinear flight dynamics problems. Prog. Aerospace Sci., 33: 539-586, 1997.
-
(1997)
Prog. Aerospace Sci
, vol.33
, pp. 539-586
-
-
Goman, M.G.1
Zagainov, G.I.2
Khramtsovsky, A.V.3
-
9
-
-
84982318349
-
Bifurcation analysis of a highly augmented aircraft model
-
USA, AIAA-96-3367-CP, American Institute of Aeronautics and Astronautics
-
G. Avanzini and G. de Matteis. Bifurcation analysis of a highly augmented aircraft model. In AIAA Atmospheric Flight Mechanics Conference Technical Papers, pages 60-68, USA, 1996. AIAA-96-3367-CP, American Institute of Aeronautics and Astronautics.
-
(1996)
AIAA Atmospheric Flight Mechanics Conference Technical Papers
, pp. 60-68
-
-
Avanzini, G.1
de Matteis, G.2
-
10
-
-
84982318243
-
Bifurcation analysis of a high incidence aircraft with nonlinear dynamic inversion control
-
USA, AIAA-97-3717-CP, American Institute of Aeronautics and Astronautics
-
D. M. Littleboy and P. R. Smith. Bifurcation analysis of a high incidence aircraft with nonlinear dynamic inversion control. In AIAA Atmospheric Flight Mechanics Conference Technical Papers, pages 629-639, USA, 1997. AIAA-97-3717-CP, American Institute of Aeronautics and Astronautics.
-
(1997)
AIAA Atmospheric Flight Mechanics Conference Technical Papers
, pp. 629-639
-
-
Littleboy, D.M.1
Smith, P.R.2
-
11
-
-
84982318687
-
Wing rock suppression in the F-15 aircraft
-
USA, AIAA-97-3719-CP, American Institute of Aeronautics and Astronautics
-
B. S. Liebst and B. R. de Witt. Wing rock suppression in the F-15 aircraft. In AIAA Atmospheric Flight Mechanics Conference Technical Papers, pages 640-652, USA, 1997. AIAA-97-3719-CP, American Institute of Aeronautics and Astronautics.
-
(1997)
AIAA Atmospheric Flight Mechanics Conference Technical Papers
, pp. 640-652
-
-
Liebst, B.S.1
de Witt, B.R.2
-
12
-
-
84983160306
-
Nonlinear analysis of the stability and control for an F-16 configuration
-
USA, AIAA-97-3722-CP, American Institute of Aeronautics and Astronautics
-
Z. Wang, Z. He, and C. E. Lan. Nonlinear analysis of the stability and control for an F-16 configuration. In AIAA Atmospheric Flight Mechanics Conference Technical Papers, pages 673-683, USA, 1997. AIAA-97-3722-CP, American Institute of Aeronautics and Astronautics.
-
(1997)
AIAA Atmospheric Flight Mechanics Conference Technical Papers
, pp. 673-683
-
-
Wang, Z.1
He, Z.2
Lan, C.E.3
-
14
-
-
84983154349
-
Global stability analysis of nonlinear aircraft dynamics
-
USA, AIAA-97-3721-CP, American Institute of Aeronautics and Astronautics
-
M. G. Goman and A. V. Khramtsovsky. Global stability analysis of nonlinear aircraft dynamics. In AIAA Atmospheric Flight Mechanics Conference Technical Papers, pages 662-672, USA, 1997. AIAA-97-3721-CP, American Institute of Aeronautics and Astronautics.
-
(1997)
AIAA Atmospheric Flight Mechanics Conference Technical Papers
, pp. 662-672
-
-
Goman, M.G.1
Khramtsovsky, A.V.2
-
15
-
-
0030214059
-
The X-31 aircraft: Advances in aircraft agility and performance
-
C. W. Alcorn, M. A. Croom, M. S. Francis, and H. Ross. The X-31 aircraft: advances in aircraft agility and performance. Prog. Aerospace Sci., 32: 377-413, 1996.
-
(1996)
Prog. Aerospace Sci
, vol.32
, pp. 377-413
-
-
Alcorn, C.W.1
Croom, M.A.2
Francis, M.S.3
Ross, H.4
-
16
-
-
84983201887
-
Bifurcation analysis as a tool for post departure stability enhancement
-
USA, AIAA-97-3716-CP, American Institute of Aeronautics and Astronautics
-
M. H. Lowenberg. Bifurcation analysis as a tool for post departure stability enhancement. In AIAA Atmospheric Flight Mechanics Conference Technical Papers, pages 615-628, USA, 1997. AIAA-97-3716-CP, American Institute of Aeronautics and Astronautics.
-
(1997)
AIAA Atmospheric Flight Mechanics Conference Technical Papers
, pp. 615-628
-
-
Lowenberg, M.H.1
-
17
-
-
3042896154
-
Bifurcation analysis of multiple-attractor flight dynamics
-
to be published in October
-
M. H. Lowenberg. Bifurcation analysis of multiple-attractor flight dynamics. Phil. Trans. R. Soc. Lon. A, to be published in October, 1998.
-
(1998)
Phil. Trans. R. Soc. Lon. A
-
-
Lowenberg, M.H.1
-
18
-
-
85027083132
-
Non-linear oscillations and chaotic behaviour in aircraft dynamics. In
-
Paper no. 6, S.A. Institute of Aeronautical Engineers
-
M. H. Lowenberg. Non-linear oscillations and chaotic behaviour in aircraft dynamics. In Proceedings of the 3rd South African Aeronautical Engineering Conference, pages 6. 1-6. 19. Paper no. 6, S. A. Institute of Aeronautical Engineers, 1991.
-
(1991)
Proceedings of the 3rd South African Aeronautical Engineering Conference
, pp. 6.1-6.19
-
-
Lowenberg, M.H.1
-
22
-
-
84983142389
-
-
Technical report, Systems Technology Inc., Technical Rept. AFWAL-TR-80-3141 Part III, USA
-
D. G. Mitchell, T. T. Myers, G. L. Teper, and D. E. Johnston. Investigation of High Angle of Attack Maneuver-Limiting Factors-Part III: Appendix I. Technical report, Systems Technology Inc., Technical Rept. AFWAL-TR-80-3141 Part III, USA, 1980.
-
(1980)
Investigation of High Angle of Attack Maneuver-Limiting Factors-Part III: Appendix I
-
-
Mitchell, D.G.1
Myers, T.T.2
Teper, G.L.3
Johnston, D.E.4
-
23
-
-
3043001368
-
Shilnikov homoclinic dynamics and the escape from roll autorotation in an f-4 model
-
be published in October
-
M. H. Lowenberg and A. R. Champneys. Shilnikov homoclinic dynamics and the escape from roll autorotation in an f-4 model. Phil. Trans. R. Soc. Lon. A, to be published in October, 1998.
-
(1998)
Phil. Trans. R. Soc. Lon. A, to
-
-
Lowenberg, M.H.1
Champneys, A.R.2
|