-
1
-
-
18844387150
-
-
Prentice-Hall, Upper Saddle River, NJ
-
Dorf, Richard, C., and Bishop, Robert, H., Modern Control Systems, 9th ed., Prentice-Hall, Upper Saddle River, NJ, 2001, pp. 553-630.
-
(2001)
Modern Control Systems, 9th Ed.
, pp. 553-630
-
-
Dorf, R.C.1
Bishop, R.H.2
-
2
-
-
0004044108
-
-
Wiley, New York
-
Stevens, B., and Lewis, F., Aircraft Control and Simulation, Wiley, New York, 1992, pp. 236-331.
-
(1992)
Aircraft Control and Simulation
, pp. 236-331
-
-
Stevens, B.1
Lewis, F.2
-
3
-
-
84978285700
-
Dynamic Inversion Applied to the F-117A
-
AIAA, Reston, VA
-
Colgren, R., and Enns, D., "Dynamic Inversion Applied to the F-117A," Proceedings of the AIAA Modeling and Simulation Technologies Conference, AIAA, Reston, VA, 1997, pp. 275-284.
-
(1997)
Proceedings of the AIAA Modeling and Simulation Technologies Conference
, pp. 275-284
-
-
Colgren, R.1
Enns, D.2
-
4
-
-
0003096706
-
Dynamic Inversion: An Evolving Methodology for Flight Control Design
-
Enns, D., Bugajski, D., Hendrick, R., and Stein, G., "Dynamic Inversion: An Evolving Methodology for Flight Control Design," International Journal of Control, Vol. 59, No. 1, 1994, pp. 71-91.
-
(1994)
International Journal of Control
, vol.59
, Issue.1
, pp. 71-91
-
-
Enns, D.1
Bugajski, D.2
Hendrick, R.3
Stein, G.4
-
5
-
-
0028467119
-
Design of Nonlinear Control Laws for High-Angle-of-Attack Flight
-
Adams, R. J., Buffington, J. M., and Banda, S. V., "Design of Nonlinear Control Laws for High-Angle-of-Attack Flight," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, 1994, pp. 737-746.
-
(1994)
Journal of Guidance, Control, and Dynamics
, vol.17
, Issue.4
, pp. 737-746
-
-
Adams, R.J.1
Buffington, J.M.2
Banda, S.V.3
-
6
-
-
0027617350
-
Robust Flight Control Design Using Dynamics Inversion and Structured Singular Value Synthesis
-
Adams, R. J., and Banda, S. V., "Robust Flight Control Design Using Dynamics Inversion and Structured Singular Value Synthesis," IEEE Transactions on Control Systems Technology, Vol. 1, No. 2, 1993, pp. 80-92.
-
(1993)
IEEE Transactions on Control Systems Technology
, vol.1
, Issue.2
, pp. 80-92
-
-
Adams, R.J.1
Banda, S.V.2
-
7
-
-
84959100701
-
Dynamic Inversion and Model-Following Control
-
AIAA, Reston, VA
-
Durham, W. C., "Dynamic Inversion and Model-Following Control, " Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 1996, pp. 1-12.
-
(1996)
Proceedings of the AIAA Guidance, Navigation, and Control Conference
, pp. 1-12
-
-
Durham, W.C.1
-
8
-
-
0141982284
-
Flight Test Experience of a Non-Linear Dynamic Inversion Control Law on the VAAC Harrier
-
AIAA Paper 3914, Aug
-
Smith, P., and Berry, A., "Flight Test Experience of a Non-Linear Dynamic Inversion Control Law on the VAAC Harrier." AIAA Paper 2000-3914, Aug. 2000.
-
(2000)
AIAA Paper
-
-
Smith, P.1
Berry, A.2
-
9
-
-
0141947704
-
Force and Moment Approach for Achievable Dynamics Using Nonlinear Dynamic Inversion
-
AIAA, Reston, VA
-
Ostroff, A. J., and Bacon, B. J., "Force and Moment Approach for Achievable Dynamics Using Nonlinear Dynamic Inversion," Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, Reston, VA, 1999, pp. 424-434.
-
(1999)
Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit
, pp. 424-434
-
-
Ostroff, A.J.1
Bacon, B.J.2
-
10
-
-
0030290057
-
Stability and Flying Qualities Robustness of a Dynamic Inversion Aircraft Control Law
-
Brinker, J. S., and Wise, K. A., "Stability and Flying Qualities Robustness of a Dynamic Inversion Aircraft Control Law,'' Journal of Guidance, Control, and Dynamics, Vol. 19, No. 6, 1996, pp. 1270-1277.
-
(1996)
Journal of Guidance, Control, and Dynamics
, vol.19
, Issue.6
, pp. 1270-1277
-
-
Brinker, J.S.1
Wise, K.A.2
-
11
-
-
0141878554
-
-
honey well Technology Center, Lockheed Martin Skunk Works, and Lockheed Martin Tactical Aircraft Systems, Wright Lab., Wl-tr-96-3099, Wright-patterson Afb, Oh, May
-
Honey well Technology Center, Lockheed Martin Skunk Works, and Lockheed Martin Tactical Aircraft Systems, "application of Multivariable Control Theory to Aircraft Control Laws: Final Report: Multivariable Control Design Guidelines, Flight Dynamics Directorate," Wright Lab., Wl-tr-96-3099, Wright-patterson Afb, Oh, May 1996.
-
(1996)
Application of Multivariable Control Theory to Aircraft Control Laws: Final Report: Multivariable Control Design Guidelines, Flight Dynamics Directorate
-
-
-
12
-
-
84959177312
-
An Approach to Select Desired Dynamics Gains for Dynamic Inversion Control Laws
-
AIAA, Reston, VA
-
Fer, H., and Enns, D.F., "An Approach to Select Desired Dynamics Gains for Dynamic Inversion Control Laws," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 1997, pp. 755-769.
-
(1997)
Proceedings of the AIAA Guidance, Navigation, and Control Conference
, pp. 755-769
-
-
Fer, H.1
Enns, D.F.2
-
13
-
-
0029210924
-
Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft
-
Reiner, J., Balas, G.J., and Garrard, W.L., "Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft," Journal of Guidance, Control and Dynamics, Vol. 18, No. 1, 1995, pp. 18-24.
-
(1995)
Journal of Guidance, Control and Dynamics
, vol.18
, Issue.1
, pp. 18-24
-
-
Reiner, J.1
Balas, G.J.2
Garrard, W.L.3
-
14
-
-
0031237430
-
Robust Longitudinal Control Design Using Dynamic Inversion and Quantitative Feedback Theory
-
Snell, S.A., and Stout, P.W., "Robust Longitudinal Control Design Using Dynamic Inversion and Quantitative Feedback Theory," Journal of Guidance, Control, and Dynamics. Vol. 20, No. 5, 1997, pp. 933-940.
-
(1997)
Journal of Guidance, Control, and Dynamics
, vol.20
, Issue.5
, pp. 933-940
-
-
Snell, S.A.1
Stout, P.W.2
-
15
-
-
29744468493
-
-
M.S. Thesis, Aerospace Engineering Dept., Texas A&M Univ., College Station, TX, Aug
-
Georgie, Jennifer, "Selection of Desired Dynamics for Dynamic Inversion Controlled Re-Entry Vehicles,"M.S. Thesis, Aerospace Engineering Dept., Texas A&M Univ., College Station, TX, Aug. 2001, pp. 13-16.
-
(2001)
Selection of Desired Dynamics for Dynamic Inversion Controlled Re-Entry Vehicles
, pp. 13-16
-
-
Georgie, J.1
-
16
-
-
0003093484
-
Preliminary Assessment of the Robustness of Dynamic Inversion Based Flight Control Laws
-
AIAA, Washington. DC
-
Snell, S.A., "Preliminary Assessment of the Robustness of Dynamic Inversion Based Flight Control Laws," Proceedings of the AIAA Guidance, Navigation and Control Conference, AIA3A, Washington. DC, 1992, pp. 206-216.
-
(1992)
Proceedings of the AIAA Guidance, Navigation and Control Conference
, pp. 206-216
-
-
Snell, S.A.1
-
18
-
-
0022059319
-
Robust Pole Assignment in Linear State Feedback
-
Kautsky, J., Nichols, N.K., and Van Dooren, P., "Robust Pole Assignment in Linear State Feedback," International Journal of Control. Vol. 41, No. 5, 1985, pp. 1129-1155.
-
(1985)
International Journal of Control
, vol.41
, Issue.5
, pp. 1129-1155
-
-
Kautsky, J.1
Nichols, N.K.2
Van Dooren, P.3
-
19
-
-
0003954806
-
-
AIAA, Washington, DC
-
Junkins, J.L., and Kim, Y., Introduction to Dynamics and Control of Flexible Structures, AIAA, Washington, DC, 1993, pp. 256-259.
-
(1993)
Introduction to Dynamics and Control of Flexible Structures
, pp. 256-259
-
-
Junkins, J.L.1
Kim, Y.2
-
20
-
-
0141947703
-
-
NASA, Johnson Space Center, Internal Memo, Clear Lake, TX, Oct
-
Shuttle Engineering Simulator X-38 V201 Actuator File," NASA, Johnson Space Center, Internal Memo, Clear Lake, TX, Oct. 1998.
-
(1998)
Shuttle Engineering Simulator X-38 V201 Actuator File
-
-
-
21
-
-
0141947702
-
-
NASA TM X-3295, Aug
-
Richards, L.G., Kuhlthau, A.R., and Jacobson, I.D., "Passenger Ride Quality from Commercial Airline Flights," NASA TM X-3295, Aug. 1975, pp. 409-436.
-
(1975)
Passenger Ride Quality from Commercial Airline Flights
, pp. 409-436
-
-
Richards, L.G.1
Kuhlthau, A.R.2
Jacobson, I.D.3
-
22
-
-
0141947697
-
-
NASA TM-X-3295, Nov
-
Duncan, N.C., and Conley, H.W., "Demographic and Psychological Variables Affecting Test Subject Evaluations of Ride Quality," NASA TM-X-3295, Nov. 1975, pp. 287-321.
-
(1975)
Demographic and Psychological Variables Affecting Test Subject Evaluations of Ride Quality
, pp. 287-321
-
-
Duncan, N.C.1
Conley, H.W.2
-
23
-
-
0141878555
-
Robust Dynamic Inversion Controller Design and Analysis to the X-38 Vehicle
-
AIAA Paper 4380
-
Ito, D., and Valasek, J., "Robust Dynamic Inversion Controller Design and Analysis to the X-38 Vehicle." AIAA Paper 2001-4380, Aug. 2001.
-
(2001)
AIAA Paper
-
-
Ito, D.1
Valasek, J.2
-
24
-
-
0024689932
-
Analysis of a Candidate Control Algorithm for a Ride-Quality Augmentation System
-
Suikat, R., Donaldson, K., and Downing, D., "Analysis of a Candidate Control Algorithm for a Ride-Quality Augmentation System," Journal of Guidance, Control, and Dynamics, Vol. 12, No. 4, 1989, pp. 505-513.
-
(1989)
Journal of Guidance, Control, and Dynamics
, vol.12
, Issue.4
, pp. 505-513
-
-
Suikat, R.1
Donaldson, K.2
Downing, D.3
-
25
-
-
0003658586
-
-
McGraw-Hill, New York
-
Nelson, Robert, C., Flight Stability and Automatic Control, 2nd ed., McGraw-Hill, New York, 1989, pp. 78-81.
-
(1989)
Flight Stability and Automatic Control, 2nd Ed.
, pp. 78-81
-
-
Nelson, R.C.1
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