-
1
-
-
0024754481
-
Design of a helicopter output feedback control law using modal and structured-robustness technique
-
Apkarian P., Champetier C., Margni J.F. Design of a helicopter output feedback control law using modal and structured-robustness technique. Internat. J. Control. 50:(4):1989.
-
(1989)
Internat. J. Control
, vol.50
, Issue.4
-
-
Apkarian, P.1
Champetier, C.2
Margni, J.F.3
-
4
-
-
0022559425
-
Optimization of control parameters for genetic algorithms
-
Grefenstette J.J. Optimization of control parameters for genetic algorithms. IEEE Trans. Systems Man Cybernet. 1986;122-128.
-
(1986)
IEEE Trans. Systems Man Cybernet.
, pp. 122-128
-
-
Grefenstette, J.J.1
-
5
-
-
0027627729
-
Linear quadratic Gaussian/loop transfer recovery design for a helicopter in low-speed flight
-
Gribble J.J. Linear quadratic Gaussian/loop transfer recovery design for a helicopter in low-speed flight. J. Guidance, Control, and Dynamics. 16:(4):1993.
-
(1993)
J. Guidance, Control, and Dynamics
, vol.16
, Issue.4
-
-
Gribble, J.J.1
-
6
-
-
0027627099
-
Quantitative feedback theory applied to the design of a rotorcraft flight control system
-
Hess R.A., Gorder P.J. Quantitative feedback theory applied to the design of a rotorcraft flight control system. J. Guidance, Control, and Dynamics. 16:(4):1993.
-
(1993)
J. Guidance, Control, and Dynamics
, vol.16
, Issue.4
-
-
Hess, R.A.1
Gorder, P.J.2
-
8
-
-
0004121705
-
-
Ph.D. Dissertation, National Cheng Kung University, Taiwan
-
∞ flight control and applications, Ph.D. Dissertation, National Cheng Kung University, Taiwan, 2000.
-
(2000)
∞ Flight Control and Applications
-
-
Kung, C.C.1
-
9
-
-
0027205718
-
The complex structured singular value
-
Packard A., Doyle J.C. The complex structured singular value. Automatica. 29:1993;71-109.
-
(1993)
Automatica
, vol.29
, pp. 71-109
-
-
Packard, A.1
Doyle, J.C.2
-
13
-
-
0029772257
-
Full envelope flight control system design using quantitative feedback theory
-
Reynolds O.R., Pachter M., Houpis C.H. Full envelope flight control system design using quantitative feedback theory. J. Guidance, Control, and Dynamics. 19:(1):1996;23-29.
-
(1996)
J. Guidance, Control, and Dynamics
, vol.19
, Issue.1
, pp. 23-29
-
-
Reynolds, O.R.1
Pachter, M.2
Houpis, C.H.3
-
16
-
-
0028548575
-
∞ helicopter flight control low design with and without rotor state feedback
-
∞ helicopter flight control low design with and without rotor state feedback. J. Guidance, Control, and Dynamics. 17:(6):1994.
-
(1994)
J. Guidance, Control, and Dynamics
, vol.17
, Issue.6
-
-
Takahashi, M.D.1
-
19
-
-
85002794339
-
Benchmark problem for robust control design
-
Wei B., Bernstein D.S. Benchmark problem for robust control design. J. Guidance, Control, and Dynamics. 15:(5):1992;1057-1059.
-
(1992)
J. Guidance, Control, and Dynamics
, vol.15
, Issue.5
, pp. 1057-1059
-
-
Wei, B.1
Bernstein, D.S.2
-
21
-
-
0025430486
-
∞ -optimisation
-
∞ -optimisation. IEEE Proceedings D. 137:(3):1990.
-
(1990)
IEEE Proceedings D
, vol.137
, Issue.3
-
-
Yue, A.1
|