-
1
-
-
84995611815
-
Decoupling of a Class of Nonlinear Systems and its Applications to an Aircraft Control Problem
-
Dec
-
Asseo, S. J., 1973, “Decoupling of a Class of Nonlinear Systems and its Applications to an Aircraft Control Problem,” Journal of Aircraft, Dec.
-
(1973)
Journal of Aircraft
-
-
Asseo, S.J.1
-
2
-
-
85025222479
-
Robust, Nonlinear, High Angle-of-Attack Control Design for a Supermaneuverable Vehicle
-
Washington DC
-
Buffington, J. M., Adams, R. J., and Banda, S. S., 1993, “Robust, Nonlinear, High Angle-of-Attack Control Design for a Supermaneuverable Vehicle,” AIAA Paper 93-3774, Washington DC.
-
(1993)
AIAA Paper 93-3774
-
-
Buffington, J.M.1
Adams, R.J.2
Banda, S.S.3
-
3
-
-
0026856998
-
Nonlinear Control Law with Application to High Angle-of-Attack Flight
-
May-June
-
Bugajski, D. J., and Enns, D. F., 1992, “Nonlinear Control Law with Application to High Angle-of-Attack Flight,” J. Guidance, Control and Dynamics, Vol. 15, No. 3, pp. 761-767, May-June.
-
(1992)
J. Guidance, Control and Dynamics
, vol.15
, Issue.3
, pp. 761-767
-
-
Bugajski, D.J.1
Enns, D.F.2
-
4
-
-
0004073353
-
-
3rd Ed., McGraw-Hill, New York
-
D’Azzo, J. J., and Houpis, C. H., 1988, Linear Control System Analysis and Design, 3rd Ed., McGraw-Hill, New York.
-
(1988)
Linear Control System Analysis and Design
-
-
D’ Azzo, J.J.1
Houpis, C.H.2
-
5
-
-
3743054240
-
Control of Nonlinear Systems and Application to Aircraft
-
University of Minnesota
-
Elgersma, M. R., 1988, “Control of Nonlinear Systems and Application to Aircraft,” Doctoral thesis, University of Minnesota.
-
(1988)
Doctoral Thesis
-
-
Elgersma, M.R.1
-
6
-
-
84999027758
-
Robustness of Dynamic Inversion vs Mu Synthesis: Lateral-Directional Example
-
Portland OR, Aug
-
Enns, D. F., 1990, “Robustness of Dynamic Inversion vs Mu Synthesis: Lateral-Directional Example,” Proceedings of the AIAA, Guidance, Navigation and Control Conference, Portland OR, Aug.
-
(1990)
Proceedings of the AIAA, Guidance, Navigation and Control Conference
-
-
Enns, D.F.1
-
7
-
-
4243069953
-
X-31 An International Success Story
-
Feb
-
Francis, M.S., 1995, “X-31 An International Success Story,” Aerospace America, Feb., pp. 22-32.
-
(1995)
Aerospace America
, pp. 22-32
-
-
Francis, M.S.1
-
8
-
-
0020191066
-
Plant Rational Transfer Function Approximation from Input-Output Data
-
Golubev, B., and Horowitz, I. M., 1982, “Plant Rational Transfer Function Approximation from Input-Output Data,” Int. J. Control, Vol. 36, pp. 711-23.
-
(1982)
Int. J. Control
, vol.36
, pp. 711-723
-
-
Golubev, B.1
Horowitz, I.M.2
-
9
-
-
0027627099
-
Quantitative Feedback Theory Applied to the Design of a Rotorcraft Flight Control System
-
Jul.-Aug
-
Hess, R. A., and Gorder, P. J., 1993, “Quantitative Feedback Theory Applied to the Design of a Rotorcraft Flight Control System,” J. Guidance, Control and Dynamics, Vol. 18, No. 4, pp. 748-753, Jul.-Aug.
-
(1993)
J. Guidance, Control and Dynamics
, vol.18
, Issue.4
, pp. 748-753
-
-
Hess, R.A.1
Gorder, P.J.2
-
10
-
-
0043243132
-
Nonlinear Controller Design for Flight Control Systems
-
University of California, Berkeley, Electronics Research Laboratory
-
Hauser, J., Sastry, S., and Meyer, G., 1988, “Nonlinear Controller Design for Flight Control Systems,” University of California, Berkeley, Electronics Research Laboratory, Memorandum UCB/ERL M88/76.
-
(1988)
Memorandum UCB/ERL M88/76
-
-
Hauser, J.1
Sastry, S.2
Meyer, G.3
-
12
-
-
85025200914
-
-
QFT Publications, Boulder, Colorado
-
Horowitz, I. M., 1993, Quantitative Feedback Design Theory (QFT) Vol. 1, QFT Publications, Boulder, Colorado.
-
(1993)
Quantitative Feedback Design Theory (QFT)
, vol.1
-
-
Horowitz, I.M.1
-
14
-
-
0019554671
-
Nonlinear Decoupling Control via Feedback: A Geometric Approach
-
AC26 #2, Apr
-
Isidori, A., Krener, A. J., Gori-Giorgi, C., and Monaco, S., 1981, “Nonlinear Decoupling Control via Feedback: A Geometric Approach,” IEEE Transactions. AC26 #2, Apr., pp. 331-345.
-
(1981)
IEEE Transactions
, pp. 331-345
-
-
Isidori, A.1
Krener, A.J.2
Gori-Giorgi, C.3
Monaco, S.4
-
15
-
-
0022679659
-
An Interpretation of Airplane General Motion and Control as an Inverse Problem
-
Mar.-Apr
-
Kato, O., and Sugiura, L., 1986, “An Interpretation of Airplane General Motion and Control as an Inverse Problem,” J. Guidance, Control and Dynamics, Mar.-Apr.
-
(1986)
J. Guidance, Control and Dynamics
-
-
Kato, O.1
Sugiura, L.2
-
16
-
-
0023089226
-
Nonlinear Flight Test Trajectory Controls for Aircraft
-
Menon, P. K. A., Badgett, M. E., Walker, R. A., and Duke, E. L., 1987, “Nonlinear Flight Test Trajectory Controls for Aircraft,” J. Guidance, Control and Dynamics, Vol. 10, No. 1, pp. 67-72.
-
(1987)
J. Guidance, Control and Dynamics
, vol.10
, Issue.1
, pp. 67-72
-
-
Menon, P.K.A.1
Badgett, M.E.2
Walker, R.A.3
Duke, E.L.4
-
17
-
-
85025209904
-
Nonlinear Flying Qualities Parameters Based on Dynamic Inversion
-
Morton, B. G., Elgersma, M. R., Harvey, C. A., and Hines, G., 1987, “Nonlinear Flying Qualities Parameters Based on Dynamic Inversion,” AFWAL-TR-87-3079.
-
(1987)
AFWAL-TR-87-3079
-
-
Morton, B.G.1
Elgersma, M.R.2
Harvey, C.A.3
Hines, G.4
-
18
-
-
85040158804
-
Simulator Study of Stall/Post Stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability
-
Dec
-
Nguyen, L. T. et al., 1979, “Simulator Study of Stall/Post Stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability,” NASA Tech Paper 1538, Dec.
-
(1979)
NASA Tech Paper 1538
-
-
Nguyen, L.T.1
-
19
-
-
0029210924
-
Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft
-
Jan-Feb
-
Reiner, J., Balas, G. J., and Garrard, W. L., 1995, “Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft,” J. Guidance Control Dynamics, Vol. 18, No. 1, pp. 18-24, Jan-Feb.
-
(1995)
J. Guidance Control Dynamics
, vol.18
, Issue.1
, pp. 18-24
-
-
Reiner, J.1
Balas, G.J.2
Garrard, W.L.3
-
20
-
-
0029772257
-
Full Envelope Flight Control System Design Using Qualitative Feedback Theory
-
Jan.-Feb
-
Reynolds, O. R., Pachter, M., and Houpis, C. H., 1996, “Full Envelope Flight Control System Design Using Qualitative Feedback Theory,” J. Guidance, Control and Dynamics, Vol. 19, No. 1, Jan.-Feb., 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
-
21
-
-
0026883988
-
Gain Scheduling: Potential Hazards and Possible Remedies
-
June
-
Shamma, J. S., and Athans, M., 1992, “Gain Scheduling: Potential Hazards and Possible Remedies,” Control Systems Magazine, June, pp. 101-107.
-
(1992)
Control Systems Magazine
, pp. 101-107
-
-
Shamma, J.S.1
Athans, M.2
-
22
-
-
0015476093
-
Decoupling in a Class of Nonlinear Systems by State Variable Feedback
-
Dec
-
Singh, S. N., and Rugh, W. J., 1972, “Decoupling in a Class of Nonlinear Systems by State Variable Feedback,” ASME Journal of Dynamic Systems, Measurement, and Control, Dec.
-
(1972)
ASME Journal of Dynamic Systems, Measurement, and Control
-
-
Singh, S.N.1
Rugh, W.J.2
-
23
-
-
0024111365
-
Control of Nearly Singular Decoupling Systems and Nonlinear Aircraft Maneuver
-
Nov
-
Singh, S. N., 1988, ‘.‘Control of Nearly Singular Decoupling Systems and Nonlinear Aircraft Maneuver,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 24, No. 6, Nov.
-
(1988)
IEEE Transactions on Aerospace and Electronic Systems
, vol.24
, Issue.6
-
-
Singh, S.N.1
-
24
-
-
78651063926
-
Preliminary Assessment of the Robustness of Dynamic Inversion Based Flight Control Laws
-
Washington DC
-
Snell, S. A., 1992, “Preliminary Assessment of the Robustness of Dynamic Inversion Based Flight Control Laws,” AIAA Paper 92-4330, Washington DC.
-
(1992)
AIAA Paper 92-4330
-
-
Snell, S.A.1
-
25
-
-
0026897471
-
Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft
-
July-Aug
-
Snell, S. A., Enns, D. F„ and Garrard, W. L., 1992, “Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft,” AIAA J. Guidance, Control Dynamics, Vol. 15, No. 4, July-Aug., pp. 976-984.
-
(1992)
AIAA J. Guidance, Control Dynamics
, vol.15
, Issue.4
, pp. 976-984
-
-
Snell, S.A.1
Enns, D.F.2
Garrard, W.L.3
-
26
-
-
0030241111
-
Quantitative Feedback Theory with a Scheduled Gain for Full Envelope Longitudinal Control Law
-
Sept.-Oct
-
Snell, S. A., and Stout, P. W., 1996, “Quantitative Feedback Theory with a Scheduled Gain for Full Envelope Longitudinal Control Law,” J. Guidance, Control and Dynamics, Vol. 19, No. 5, Sept.-Oct., pp. 1095-1101.
-
(1996)
J. Guidance, Control and Dynamics
, vol.19
, Issue.5
, pp. 1095-1101
-
-
Snell, S.A.1
Stout, P.W.2
|