-
1
-
-
84902330155
-
X-31, F-16 MATV, F/A-18 HARV Explore Diverse Missions
-
April 18
-
Domheim, M. A., “X-31, F-16 MATV, F/A-18 HARV Explore Diverse Missions,” Aviation Week & Space Technology, Vol. 140, April 18,1994, pp. 46-47.
-
(1994)
Aviation Week & Space Technology
, vol.140
, pp. 46-47
-
-
Domheim, M.A.1
-
2
-
-
0025539083
-
A Fixed H-a Controller for a Supermaneuverable Fighter Performing the Herbst Maneuver
-
Inst, of Electrical and Electronics Engineers, New York
-
a Controller for a Supermaneuverable Fighter Performing the Herbst Maneuver,” Proceedings of the 29th Conference on Decision and Control (Honolulu, HI), Inst, of Electrical and Electronics Engineers, New York, 1990, pp. 2599-2606.
-
(1990)
Proceedings of the 29Th Conference on Decision and Control (Honolulu, HI)
, pp. 2599-2606
-
-
Chiang, R.Y.1
Safonov, K.P.2
Tekawy, J.A.3
-
3
-
-
85003361447
-
High Performance Linear-Quadratic and Hrxt Designs for a ‘Supermaneuverable Aircraft,”
-
Voulgaris, P., and Valvani, L., “High Performance Linear-Quadratic and Hrxt Designs for a ‘Supermaneuverable’ Aircraft,” Journal of Guidance, Control, and Dynamics, Vol. 4, No. 1, 1991, pp. 157-165.
-
(1991)
Journal of Guidance, Control, and Dynamics
, vol.4
, Issue.1
, pp. 157-165
-
-
Voulgaris, P.1
Valvani, L.2
-
4
-
-
0026837210
-
High-Alpha Application of Variable Gain Output Feedback Control
-
Ostroff, A. J., “High-Alpha Application of Variable Gain Output Feedback Control,” Journal of Guidance, Control, and Dynamics, Vol. 15, No. 2, 1992, pp. 491-497.
-
(1992)
Journal of Guidance, Control, and Dynamics
, vol.15
, Issue.2
, pp. 491-497
-
-
Ostroff, A.J.1
-
5
-
-
0027657334
-
Application of Structured Singular Value Synthesis to a Fighter Aircraft
-
Sparks, A., and Siva, B., “Application of Structured Singular Value Synthesis to a Fighter Aircraft,” Journal of Guidance, Control, and Dynamics, Vol. 16, No. 5, 1994, pp. 940-947.
-
(1994)
Journal of Guidance, Control, and Dynamics
, vol.16
, Issue.5
, pp. 940-947
-
-
Sparks, A.1
Siva, B.2
-
6
-
-
0000402415
-
Decoupling in the Design and Synthesis of Multivariable Control Systems
-
Vol. AC-12
-
Falb, P. L., and Wolovich, W. A., “Decoupling in the Design and Synthesis of Multivariable Control Systems,” IEEE Transactions on Automatic Control, Vol. AC-12, No. 6, 1967, pp. 651-659.
-
(1967)
IEEE Transactions on Automatic Control
, vol.6
, pp. 651-659
-
-
Falb, P.L.1
Wolovich, W.A.2
-
7
-
-
0015476093
-
Decoupling in a Class of Nonlinear Systems by State Variable Feedback
-
Dec
-
Singh, S. N., and Rugh, W. J., “Decoupling in a Class of Nonlinear Systems by State Variable Feedback,” Journal of Dynamic Systems, Measurement, and Control, Vol. 94, Dec. 1972, pp. 323-329.
-
(1972)
Journal of Dynamic Systems, Measurement, and Control
, vol.94
, pp. 323-329
-
-
Singh, S.N.1
Rugh, W.J.2
-
8
-
-
0039899545
-
Output Feedback Nonlinear Decoupled Control Synthesis and Observer Design For Maneuvering Aircraft
-
Singh, S. N„ and Schy, A. A., “Output Feedback Nonlinear Decoupled Control Synthesis and Observer Design For Maneuvering Aircraft,” International Journal of Control, Vol. 31, No. 4, 1980, pp. 781-806.
-
(1980)
International Journal of Control
, vol.31
, Issue.4
, pp. 781-806
-
-
Singh, S.N.1
Schy, A.A.2
-
9
-
-
84912676085
-
Application of Nonlinear Systems Inverses to Automatic Flight Control Design—System Concept and Flight Evaluations
-
AGARD, AG251
-
Meyer, G., and Cicolani, L., “Application of Nonlinear Systems Inverses to Automatic Flight Control Design—System Concept and Flight Evaluations,” Theory and Application of Optimal Control in Aerospace Systems, AGARD, AG251, 1981, pp. 10.1-10.29.
-
(1981)
Theory and Application of Optimal Control in Aerospace Systems
, pp. 10.1-10.29
-
-
Meyer, G.1
Cicolani, L.2
-
10
-
-
0021156774
-
Application of Nonlinear Transformations to Automatic Flight Control
-
Meyer, G., Su, R., and Hunt, R., “Application of Nonlinear Transformations to Automatic Flight Control,” Automatica, Vol. 20, No. 1,1984, pp. 103-107.
-
(1984)
Automatica
, vol.20
, Issue.1
, pp. 103-107
-
-
Meyer, G.1
Su, R.2
Hunt, R.3
-
11
-
-
85003269298
-
Nonlinear Flight Test Trajectory Controllers for Aircraft
-
AIAA, New York, AIAA Paper 85-1890
-
Menon, P. K., Badgett, M. E., and Walker, R. A.,“Nonlinear Flight Test Trajectory Controllers for Aircraft,” Proceedings of the AIAA Guidance and Control Conference (Snow Mass, CO), AIAA, New York, 1985, pp. 481-489 (AIAA Paper 85-1890).
-
(1985)
Proceedings of the AIAA Guidance and Control Conference (Snow Mass, CO)
, pp. 481-489
-
-
Menon, P.K.1
Badgett, M.E.2
Walker, R.A.3
-
12
-
-
84995611815
-
Decoupling of a Class of Nonlinear Systems and Its Application to an Aircraft Control Problem
-
Asseo, S. J., “Decoupling of a Class of Nonlinear Systems and Its Application to an Aircraft Control Problem,” Journal of Aircraft, Vol. 10, No. 12, 1973, pp. 739-747.
-
(1973)
Journal of Aircraft
, vol.10
, Issue.12
, pp. 739-747
-
-
Asseo, S.J.1
-
13
-
-
0024051348
-
Flight Control Design Using Nonlinear Inverse Dynamics
-
Lane, S. H„ and Stengel, R. F., “Flight Control Design Using Nonlinear Inverse Dynamics,” Automatica, Vol. 24, No. 4, 1988. pp. 471-483.
-
(1988)
Automatica
, vol.24
, Issue.4
, pp. 471-483
-
-
Lane, S.H.1
Stengel, R.F.2
-
14
-
-
0026897471
-
Nonlinear Inversion Flight Control for a Supermaneuver Aircraft
-
Snell, S. A., Enns, D. F., and Garrard, W. L., “Nonlinear Inversion Flight Control for a Supermaneuver Aircraft,” Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp. 976-984.
-
(1992)
Journal of Guidance, Control, and Dynamics
, vol.15
, Issue.4
, pp. 976-984
-
-
Snell, S.A.1
Enns, D.F.2
Garrard, W.L.3
-
15
-
-
0026856998
-
Nonlinear Control Law with Application to High Angle-of-Attack Flight
-
Bugajski, D. J., and Enns, D. F., “Nonlinear Control Law with Application to High Angle-of-Attack Flight,” Journal of Guidance, Control, and Dynamics, Vol. 15, No. 3, 1992, pp. 761-767.
-
(1992)
Journal of Guidance, Control, and Dynamics
, vol.15
, Issue.3
, pp. 761-767
-
-
Bugajski, D.J.1
Enns, D.F.2
-
16
-
-
84992365655
-
Robust, Nonlinear, High-Angle-of-Attack Control for a Supermaneuverable Vehicle
-
AIAA, Washington, DC, AIAA Paper 93-3774
-
Buffington, J., Adams, R„ and Banda, S., “Robust, Nonlinear, High-Angle-of-Attack Control for a Supermaneuverable Vehicle,” Proceedings of the AIAA Guidance, Navigation, and Control Conference (Monterey, CA), AIAA, Washington, DC, 1993, pp. 690-700 (AIAA Paper 93-3774).
-
(1993)
Proceedings of the AIAA Guidance, Navigation, and Control Conference (Monterey, CA)
, pp. 690-700
-
-
Buffington, J.1
Adams, R.2
Banda, S.3
-
17
-
-
3743054240
-
-
Doctoral Thesis, Dept, of Electrical Engineering, Univ. of Minnesota, Minneapolis, MN
-
Elgersma, M. R., “Control of Nonlinear Systems and Application to Aircraft,” Doctoral Thesis, Dept, of Electrical Engineering, Univ. of Minnesota, Minneapolis, MN, 1988.
-
(1988)
Control of Nonlinear Systems and Application to Aircraft
-
-
Elgersma, M.R.1
-
18
-
-
0004099251
-
-
Prentice-Hall, Englewood Cliffs, NJ
-
Slotine, J. E., and Li, W., Applied Nonlinear Control, Prentice-Hall, Englewood Cliffs, NJ, 1991.
-
(1991)
Applied Nonlinear Control
-
-
Slotine, J.E.1
Li, W.2
-
19
-
-
0000831881
-
Robust Dynamic Inversion Control Law for Aircraft Control
-
AIAA, Washington, DC
-
Balas, G. J., Reiner, J., and Garrard, W. L., “Robust Dynamic Inversion Control Law for Aircraft Control,” Proceedings of the AIAA Guidance, Navigation, and Control Conference (Hilton Head, SC), AIAA, Washington, DC, 1992, pp. 192-205.
-
(1992)
Proceedings of the AIAA Guidance, Navigation, and Control Conference (Hilton Head, SC)
, pp. 192-205
-
-
Balas, G.J.1
Reiner, J.2
Garrard, W.L.3
-
20
-
-
85003414822
-
Design of a Flight Control System for a Highly Maneuverable Aircraft Using /x Synthesis
-
AIAA, Washington, DC
-
Balas, G. J., Reiner, J., and Garrard, W. L., “Design of a Flight Control System for a Highly Maneuverable Aircraft Using /x Synthesis,” Proceedings of the AIAA Guidance, Navigation, and Control Conference (Monterey, CA), AIAA, Washington, DC, 1993, pp. 702-710.
-
(1993)
Proceedings of the AIAA Guidance, Navigation, and Control Conference (Monterey, CA)
, pp. 702-710
-
-
Balas, G.J.1
Reiner, J.2
Garrard, W.L.3
-
21
-
-
33749935959
-
-
MUSYN, Inc., Minneapolis, MN, and The Mathworks, Natick, MA, May
-
Balas, G. J., Doyle, J. C., Glover, K., Packard A. K., and Smith, R., “The p Analysis and Synthesis Toolbox User’s Guide,” MUSYN, Inc., Minneapolis, MN, and The Mathworks, Natick, MA, May 1991.
-
(1991)
The P Analysis and Synthesis Toolbox Users Guide,”
-
-
Balas, G.J.1
Doyle, J.C.2
Glover, K.3
Packard, A.K.4
Smith, R.5
-
22
-
-
0027609973
-
“Linear, Multivariable Robust Control with a ¡x
-
Packard, A. K., Doyle, J. C., and Balas, G. J., “Linear, Multivariable Robust Control with a ¡x Perspective,” ASME Journal of Dynamics, Measurements and Control: Special Edition on Control, Vol. 115, No. 2b, 1993, pp. 426-438.
-
(1993)
ASME Journal of Dynamics, Measurements and Control: Special Edition on Control
, vol.115
, Issue.2b
, pp. 426-438
-
-
Packard, A.K.1
Doyle, J.C.2
Balas, G.J.3
-
23
-
-
0020203138
-
Analysis of Feedback Systems with Structured Uncertainties
-
Doyle, J. C., “Analysis of Feedback Systems with Structured Uncertainties,” Proceedings of the Institute of Electrical and Electronics Engineers, Vol. 129, No. 6, 1982, pp. 242-250.
-
(1982)
Proceedings of the Institute of Electrical and Electronics Engineers
, vol.129
, Issue.6
, pp. 242-250
-
-
Doyle, J.C.1
-
24
-
-
0022958980
-
Design Examples Using /x Synthesis: Space Shuttle Lateral Axis FCS During Reentry
-
New York, NY
-
Doyle, J. C., Lenz, K., and Packard, A. K., “Design Examples Using /x Synthesis: Space Shuttle Lateral Axis FCS During Reentry,” Proceedings of the 25th Conference on Decision and Control, New York, NY, Dec. 1986, pp. 2218-2223.
-
(1986)
Proceedings of the 25Th Conference on Decision and Control
, pp. 2218-2223
-
-
Doyle, J.C.1
Lenz, K.2
Packard, A.K.3
-
25
-
-
0038083065
-
Lecture Notes on Advances in Multivariable Control
-
Honeywell, Inc., Minneapolis, MN, Oct
-
Doyle, J. C., “Lecture Notes on Advances in Multivariable Control,” ONR/Honeywell Workshop on Advances in Multivariable Control, Honeywell, Inc., Minneapolis, MN, Oct. 1984.
-
(1984)
Onr/Honeywell Workshop on Advances in Multivariable Control
-
-
Doyle, J.C.1
-
26
-
-
0024715909
-
State Space Solutions to Standard H
-
Doyle, J. C., Glover, K., Khargonekar, P., and Francis, B. A., “State Space Solutions to Standard H2 and H Control Problems,” IEEE Transactions on Automatic Control Vol. AC-34, No. 8, 1989, pp. 831-847.
-
(1989)
IEEE Transactions on Automatic Control
, vol.AC-34
, Issue.8
, pp. 831-847
-
-
Doyle, J.C.1
Glover, K.2
Khargonekar, P.3
Francis, B.A.4
-
28
-
-
0042949777
-
-
Ph.D. Thesis, Dept, of Aerospace Engineering and Mechanics, Univ. of Minnesota, Minneapolis, MN, July
-
Reiner, J., “Control Design for Aircraft Using Robust Dynamic Inversion Technique,” Ph.D. Thesis, Dept, of Aerospace Engineering and Mechanics, Univ. of Minnesota, Minneapolis, MN, July 1993.
-
(1993)
Control Design for Aircraft Using Robust Dynamic Inversion Technique
-
-
Reiner, J.1
-
30
-
-
85003703953
-
-
AIAA 28th Aerospace Sciences Meeting, AIAA Paper 90-0219, Reno, NV, Jan
-
Krekeler, G., Wilson, D. J., and Riley, D. R., “High Angle-of-Attack Flying Qualities Criteria,” AIAA 28th Aerospace Sciences Meeting, AIAA Paper 90-0219, Reno, NV, Jan. 1990.
-
(1990)
High Angle-Of-Attack Flying Qualities Criteria
-
-
Krekeler, G.1
Wilson, D.J.2
Riley, D.R.3
-
31
-
-
0345950504
-
-
NASA TM-107601
-
Buttrill, C. S., Arbuckle, P. D., and Hoffler, K, “Simulation Model of a Twin-Tail High Performance Airplane,” NASA TM-107601, 1992.
-
(1992)
Simulation Model of a Twin-Tail High Performance Airplane
-
-
Buttrill, C.S.1
Arbuckle, P.D.2
Hoffler, K.3
|