-
1
-
-
0032073562
-
Agile missile dynamics and control
-
Wise K A, Broy D J. Agile missile dynamics and control[J]. Journal of Guidance, Control and Dynamics, 1998, 21(3): 441-449.
-
(1998)
Journal of Guidance, Control and Dynamics
, vol.21
, Issue.3
, pp. 441-449
-
-
Wise, K.A.1
Broy, D.J.2
-
2
-
-
33846595590
-
Augmentation of high-altitude maneuver performance of tail-controlled missile using lateral thrust
-
ADA-328973
-
Chadwick K A. Augmentation of high-altitude maneuver performance of tail-controlled missile using lateral thrust[R]. ADA-328973, 1997.
-
(1997)
-
-
Chadwick, K.A.1
-
3
-
-
33748205273
-
Autopilot design for agile missile with aerodynamic fin and side thruster
-
Japan, Fukui: IEEC Press
-
Yong S C, Choi C L, Jae W C. Autopilot design for agile missile with aerodynamic fin and side thruster[C]//SICE Annual Conference. Japan, Fukui: IEEC Press, 2003: 1476-1481.
-
(2003)
SICE Annual Conference
, pp. 1476-1481
-
-
Yong, S.C.1
Choi, C.L.2
Jae, W.C.3
-
5
-
-
33748159886
-
Side jet and aerodynamics compound control system design of air defense missiles
-
in Chinese
-
Cheng F Z, Wan Z M, Chen S L, et al. Side jet and aerodynamics compound control system design of air defense missiles[J]. Flight Dynamics, 2003, 21(2): 49-52. (in Chinese)
-
(2003)
Flight Dynamics
, vol.21
, Issue.2
, pp. 49-52
-
-
Cheng, F.Z.1
Wan, Z.M.2
Chen, S.L.3
-
6
-
-
3042677139
-
Adaptive techniques for multiple actuator blending
-
AIAA 98-4494
-
Menon P K, Iragavarapu V R. Adaptive techniques for multiple actuator blending[R]. AIAA 98-4494, 1998.
-
(1998)
-
-
Menon, P.K.1
Iragavarapu, V.R.2
-
7
-
-
0032071047
-
A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering
-
Thukral A, Innocenti M. A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering[J]. IEEE Transactions on Control Systems Technology, 1998, 6(3): 359-371.
-
(1998)
IEEE Transactions on Control Systems Technology
, vol.6
, Issue.3
, pp. 359-371
-
-
Thukral, A.1
Innocenti, M.2
-
8
-
-
0028710584
-
An appropriate application of fuzzy logic: Missile autopilot for dual control implementation
-
Columbus: IEEE Press
-
Schroeder W K, Liu K. An appropriate application of fuzzy logic: missile autopilot for dual control implementation[C]//IEEE International Symposium on Intelligent Control. Columbus: IEEE Press, 1994: 93-98.
-
(1994)
IEEE International Symposium on Intelligent Control
, pp. 93-98
-
-
Schroeder, W.K.1
Liu, K.2
-
9
-
-
85087593877
-
Autopilot design for a missile with reaction jet using coefficient diagram
-
Canada, Montreal: AIAA Press
-
Hirokawa R, Sato K. Autopilot design for a missile with reaction jet using coefficient diagram[C]//AIAA Guidance, Navigation and Control Conference and Exhibit. Canada, Montreal: AIAA Press, 2001: 1-8.
-
(2001)
AIAA Guidance, Navigation and Control Conference and Exhibit
, pp. 1-8
-
-
Hirokawa, R.1
Sato, K.2
-
10
-
-
0034230327
-
A new mutation rule for evolutionary programming motivated from back propagation learning
-
Choi D H, Oh S Y. A new mutation rule for evolutionary programming motivated from back propagation learning[J]. IEEE Transaction on Evolutionary Computation, 2000, 4(2): 188-190.
-
(2000)
IEEE Transaction on Evolutionary Computation
, vol.4
, Issue.2
, pp. 188-190
-
-
Choi, D.H.1
Oh, S.Y.2
|