-
1
-
-
84965432097
-
-
Azvine, B., Wynne, R.J., 1992. A Review of Quantitative Feedback Theory as a Robust Control System Design Technique. Transactions of the Institute of Measurement and Control 14(5), pp. 265-279.
-
(1992)
A Review of Quantitative Feedback Theory as a Robust Control System Design Technique. Transactions of the Institute of Measurement and Control
, vol.14
, Issue.5
, pp. 265-279
-
-
Azvine, B.1
Wynne, R.J.2
-
5
-
-
0028322834
-
Design of robust quantitative feedback theory controllers for pitch attitude hold systems
-
Bossert, D.E., 1994. Design of Robust Quantitative Feedback Theory Controllers for Pitch Attitude Hold Systems. J Guidance, Control, and Dynamics 17(1), pp. 217-219.
-
(1994)
J Guidance, Control, and Dynamics
, vol.17
, Issue.1
, pp. 217-219
-
-
Bossert, D.E.1
-
6
-
-
85033894759
-
Robust flight control using quantitative feedback theory: Scalar system design
-
ICC/1/96, Industrial Control Centre, University of Strathclyde
-
Breslin, S.G., Grimble, M.J., 1996. Robust Flight Control using Quantitative Feedback Theory: Scalar System Design. Technical Report, ICC/1/96, Industrial Control Centre, University of Strathclyde.
-
(1996)
Technical Report
-
-
Breslin, S.G.1
Grimble, M.J.2
-
7
-
-
85033894759
-
Robust flight control using quantitative feedback theory: Preliminary design studies
-
ICC/123/96, Industrial Control Centre, University of Strathclyde
-
Breslin, S.G., Grimble, M.J., 1996. Robust Flight Control using Quantitative Feedback Theory: Preliminary Design Studies. Technical Report, ICC/123/96, Industrial Control Centre, University of Strathclyde.
-
(1996)
Technical Report
-
-
Breslin, S.G.1
Grimble, M.J.2
-
8
-
-
0004073353
-
-
McGraw-Hill Book Company, New York
-
D'Azzo, J.J., Houpis, C.H., 1988, Linear Control System Analysis and Design: Conventional and Modern. Third Edition, McGraw-Hill Book Company, New York, pp. 686-742.
-
(1988)
Linear Control System Analysis and Design: Conventional and Modern. Third Edition
, pp. 686-742
-
-
D'Azzo, J.J.1
Houpis, C.H.2
-
10
-
-
0030242490
-
Development and flight testing of quantitative feedback theory pitch rate stability augmentation system
-
Fontenrose, P.L., Hall, C.E., 1996. Development and Flight Testing of Quantitative Feedback Theory Pitch Rate Stability Augmentation System. J. Guidance, Control, and Dynamics, 19(5), pp. 1109-1115.
-
(1996)
J. Guidance, Control, and Dynamics
, vol.19
, Issue.5
, pp. 1109-1115
-
-
Fontenrose, P.L.1
Hall, C.E.2
-
12
-
-
0016890969
-
Synthesis of feedback systems with nonlinear time uncertain plants to satisfy quantitative performance specifications
-
Horowitz, I.M., 1976. Synthesis of Feedback Systems with Nonlinear Time Uncertain Plants to Satisfy Quantitative Performance Specifications. IEEE Transactions on Automatic Control, 64, 123-130.
-
(1976)
IEEE Transactions on Automatic Control
, vol.64
, pp. 123-130
-
-
Horowitz, I.M.1
-
13
-
-
85033885782
-
-
QFT Publications, 4470-Ave., Boulder, Colorado
-
Horowitz, I.M., 1993. Quantitative Feedback Design Theory, Vol. 1, QFT Publications, 4470-Ave., Boulder, Colorado.
-
(1993)
Quantitative Feedback Design Theory
, vol.1
-
-
Horowitz, I.M.1
-
14
-
-
0015386585
-
Synthesis of feedback systems with large plant ignorance for prescribed time domain tolerance
-
Horowitz, I.M., Sidi, M., 1972. Synthesis of Feedback Systems with Large Plant Ignorance for Prescribed Time Domain Tolerance. International Journal of Control 16(2), pp. 287-309.
-
(1972)
International Journal of Control
, vol.16
, Issue.2
, pp. 287-309
-
-
Horowitz, I.M.1
Sidi, M.2
-
15
-
-
4243156632
-
Quantitative feedback theory (QFT): Technique for designing multivariabe control systems
-
AFWAL-TR-86-3107. Wright-Patterson Air Force Base, Ohio
-
Houpis, C.H., 1987. Quantitative Feedback Theory (QFT): Technique for Designing Multivariabe Control Systems. Air Force Wright Aeronautical Laboratories. AFWAL-TR-86-3107. Wright-Patterson Air Force Base, Ohio.
-
(1987)
Air Force Wright Aeronautical Laboratories
-
-
Houpis, C.H.1
-
16
-
-
0029191478
-
QFT applied to fault flight control system design
-
Keating, M.S., Pachter, M., Houpis, C.H., 1995. QFT Applied to Fault Flight Control System Design, Proceedings of ACC, pp. 184-188.
-
(1995)
Proceedings of ACC
, pp. 184-188
-
-
Keating, M.S.1
Pachter, M.2
Houpis, C.H.3
-
17
-
-
0040753000
-
-
Master Thesis, AFIT/GE/ENG/94D-24, Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio
-
Phillips, S.N., 1994. A Quantitative Feedback Theory FCS Design for the Subsonic Envelope of the VISTA F-16 Including Configuration Variation, Master Thesis, AFIT/GE/ENG/94D-24, Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio.
-
(1994)
A Quantitative Feedback Theory FCS Design for the Subsonic Envelope of the VISTA F-16 Including Configuration Variation
-
-
Phillips, S.N.1
-
18
-
-
0029772257
-
Full envelope flight control system design using quantitative feedback theory
-
Reynolds, O.R., Pachter, M., Houpis, C.H., 1996. Full Envelope Flight Control System Design Using Quantitative Feedback Theory. J Guidance, Control, and Dynamics 19(1), pp. 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
-
19
-
-
0030241111
-
Quantitative feedback theory with a scheduled gain for full envelope longitudinal control
-
Snell, S.A., Stout, P.W., 1996. Quantitative Feedback Theory with a Scheduled Gain for Full Envelope Longitudinal Control, J. Guidance, Control, and Dynamics 19(5), pp. 1095-1101
-
(1996)
J. Guidance, Control, and Dynamics
, vol.19
, Issue.5
, pp. 1095-1101
-
-
Snell, S.A.1
Stout, P.W.2
-
21
-
-
85033873216
-
-
DGLR-JT96-094, JAHRBUCH 1996I, Deutscher Luft-und Raumfahrtkongreß DGLR-Jahrestagung 1996, Dresden
-
Wu, S., Reichert, G., 1996. Design and Analysis of a Lateral Flight Control and Path Guidance System for Commercial Aircraft. DGLR-JT96-094, JAHRBUCH 1996I, pp. 493-502, Deutscher Luft-und Raumfahrtkongreß DGLR-Jahrestagung 1996, Dresden.
-
(1996)
Design and Analysis of a Lateral Flight Control and Path Guidance System for Commercial Aircraft
, pp. 493-502
-
-
Wu, S.1
Reichert, G.2
|