-
1
-
-
85003354978
-
System Identification for Adaptive and Reconfigurable Control
-
May-June
-
P. R. Chandler, M. Pachter, and M. Mears, "System Identification for Adaptive and Reconfigurable Control," Journal of Guidance, Control and Dynamics, vol. 18, pp. 516-524, May-June 1995.
-
(1995)
Journal of Guidance, Control and Dynamics
, vol.18
, pp. 516-524
-
-
Chandler, P.R.1
Pachter, M.2
Mears, M.3
-
2
-
-
0029192309
-
A Self-Designing Receding Horizon Optimal Flight Controller
-
June
-
D. Ward and R. Barron, "A Self-Designing Receding Horizon Optimal Flight Controller ," in American Control Conference, June 1995.
-
(1995)
American Control Conference
-
-
Ward, D.1
Barron, R.2
-
3
-
-
0030732624
-
Nonlinear Flight Control using Neural Networks
-
B. Kim and A. Calise, "Nonlinear Flight Control using Neural Networks," Journal of Guidance, Control and Dynamics, vol. 20, no. 1, pp. 26-33, 1997.
-
(1997)
Journal of Guidance, Control and Dynamics
, vol.20
, Issue.1
, pp. 26-33
-
-
Kim, B.1
Calise, A.2
-
4
-
-
85057639029
-
Generic Neural Flight Control and Autopilot System
-
AIAA Paper 2000-4281, August
-
J. Kaneshige, J. Bull, and J. J. Totah, "Generic Neural Flight Control and Autopilot System," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2000-4281, August 2000.
-
(2000)
AIAA Guidance, Navigation, and Control Conference
-
-
Kaneshige, J.1
Bull, J.2
Totah, J.J.3
-
5
-
-
35648944154
-
Selected Flight Test Results for On-line Learning Neural Network-Based Flight Control System,
-
Tech. Rep. TM-2004-212857, NASA, December
-
P. S. Williams-Hayes,"Selected Flight Test Results for On-line Learning Neural Network-Based Flight Control System," Tech. Rep. TM-2004-212857, NASA, December 2004.
-
(2004)
-
-
Williams-Hayes, P.S.1
-
6
-
-
35648981588
-
Flight Test Implementation of a Second Generation Intelligent Flight Control System
-
AIAA Paper 2005-6995, September
-
P. S. Williams-Hayes, "Flight Test Implementation of a Second Generation Intelligent Flight Control System," AIAA Paper 2005-6995, September 2005.
-
(2005)
-
-
Williams-Hayes, P.S.1
-
7
-
-
0035441678
-
Flight Testing of Reconfigurable Control Law on the X-36 Tailless Aircraft
-
J. S. Brinker and K. A. Wise, "Flight Testing of Reconfigurable Control Law on the X-36 Tailless Aircraft," Journal of Guidance, Control, and Dynamics, vol. 24, no. 5, pp. 903-909, 2001.
-
(2001)
Journal of Guidance, Control, and Dynamics
, vol.24
, Issue.5
, pp. 903-909
-
-
Brinker, J.S.1
Wise, K.A.2
-
8
-
-
85087605832
-
Application of an Adaptive Autopilot Design to a Family of Guided Munitions
-
AIAA Paper 2000-3969, August
-
M. Sharma, A. J. Calise, and J. E. Corban, "Application of an Adaptive Autopilot Design to a Family of Guided Munitions," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2000-3969, August 2000.
-
(2000)
AIAA Guidance, Navigation, and Control Conference
-
-
Sharma, M.1
Calise, A.J.2
Corban, J.E.3
-
9
-
-
33845749151
-
Application and Flight Testing of an Adaptive Autopilot on Precision Guided Munitions
-
AIAA Paper 2006-6568, August
-
M. Sharma, E. Lavretsky, and K. Wise, "Application and Flight Testing of an Adaptive Autopilot on Precision Guided Munitions," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2006-6568, August 2006.
-
(2006)
AIAA Guidance, Navigation, and Control Conference
-
-
Sharma, M.1
Lavretsky, E.2
Wise, K.3
-
10
-
-
0035394068
-
Comparison of Intelligent, Adaptive, and Nonlinear Flight Control Laws
-
M. Steinberg, "Comparison of Intelligent, Adaptive, and Nonlinear Flight Control Laws," Journal of Guidance, Control, and Dynamics, vol. 24, no. 4, pp. 693-699, 2001.
-
(2001)
Journal of Guidance, Control, and Dynamics
, vol.24
, Issue.4
, pp. 693-699
-
-
Steinberg, M.1
-
11
-
-
9944221596
-
Integrated Adaptive Guidance and Control for Re-Entry Vehicles with Flight Test Results
-
J. Schierman, D. Ward, J. Hull, N. Gandhi, M. Oppenheimer, and D. Doman, "Integrated Adaptive Guidance and Control for Re-Entry Vehicles with Flight Test Results," Journal of Guidance, Control, and Dynamics, vol. 27, no. 6, pp. 975-988, 2004.
-
(2004)
Journal of Guidance, Control, and Dynamics
, vol.27
, Issue.6
, pp. 975-988
-
-
Schierman, J.1
Ward, D.2
Hull, J.3
Gandhi, N.4
Oppenheimer, M.5
Doman, D.6
-
12
-
-
85003342310
-
Hybrid Approach to Nearoptimal Launch Vehicle Guidance
-
M. Leung and A. J. Calise, "Hybrid Approach to Nearoptimal Launch Vehicle Guidance," Journal of Guidance, Control, and Dynamics, vol. 17, no. 5, pp. 881-888, 1994.
-
(1994)
Journal of Guidance, Control, and Dynamics
, vol.17
, Issue.5
, pp. 881-888
-
-
Leung, M.1
Calise, A.J.2
-
13
-
-
9944256568
-
Generation of Launch Vehicle Abort Trajectories Using a Hybrid Optimization Method
-
A. J. Calise and N. Brandt, "Generation of Launch Vehicle Abort Trajectories Using a Hybrid Optimization Method," Journal of Guidance, Control, and Dynamics, vol. 27, no. 6, pp. 929-929, 2004.
-
(2004)
Journal of Guidance, Control, and Dynamics
, vol.27
, Issue.6
, pp. 929-929
-
-
Calise, A.J.1
Brandt, N.2
-
14
-
-
85079014228
-
Advanced Guidance and Control Methods for Reusable Launch Vehicles: Test Results
-
AIAA Paper 2002-4561, August
-
J. Hanson and R. Jones, "Advanced Guidance and Control Methods for Reusable Launch Vehicles: Test Results," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2002-4561, August 2002.
-
(2002)
AIAA Guidance, Navigation, and Control Conference
-
-
Hanson, J.1
Jones, R.2
-
15
-
-
2942726451
-
Test Results for Entry Guidance Methods for Reusable Launch Vehicles
-
AIAA Paper 2004-701, January
-
J. Hanson and R. Jones, "Test Results for Entry Guidance Methods for Reusable Launch Vehicles," in 42nd AIAA Aerospace Sciences Meeting, AIAA Paper 2004-701, January 2004.
-
(2004)
42nd AIAA Aerospace Sciences Meeting
-
-
Hanson, J.1
Jones, R.2
-
16
-
-
9944259104
-
Test Results for Entry Guidance Methods for Space Vehicles
-
J. M. Hanson and R. E. Jones, "Test Results for Entry Guidance Methods for Space Vehicles," Journal of Guidance, Control, and Dynamics, vol. 27, no. 6, pp. 960-966, 2004.
-
(2004)
Journal of Guidance, Control, and Dynamics
, vol.27
, Issue.6
, pp. 960-966
-
-
Hanson, J.M.1
Jones, R.E.2
-
17
-
-
85085402860
-
Performance of Evolved Acceleration Guidance Logic for Entry (EAGLE)
-
AIAA Paper 2002-4456, Aug
-
J. Leavitt, A. Saraf, D. Chen, and K. Mease, "Performance of Evolved Acceleration Guidance Logic for Entry (EAGLE)," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2002-4456, Aug. 2002.
-
(2002)
AIAA Guidance, Navigation, and Control Conference
-
-
Leavitt, J.1
Saraf, A.2
Chen, D.3
Mease, K.4
-
18
-
-
0036494491
-
Reduced-Order Entry Trajectory Planning for Acceleration Guidance
-
K. D. Mease, D. T. Chen, P. Teufel, and H. Schogravenenberger, "Reduced-Order Entry Trajectory Planning for Acceleration Guidance," Journal of Guidance, Control, and Dynamics, vol. 25, no. 2, pp. 257-266, 2002.
-
(2002)
Journal of Guidance, Control, and Dynamics
, vol.25
, Issue.2
, pp. 257-266
-
-
Mease, K.D.1
Chen, D.T.2
Teufel, P.3
Schogravenenberger, H.4
-
20
-
-
9944233154
-
Dynamic Lateral Entry Guidance Logic
-
Z. Shen and P. Lu, "Dynamic Lateral Entry Guidance Logic," Journal of Guidance, Control, and Dynamics, vol. 27, no. 6, pp. 949-959, 2004.
-
(2004)
Journal of Guidance, Control, and Dynamics
, vol.27
, Issue.6
, pp. 949-959
-
-
Shen, Z.1
Lu, P.2
-
21
-
-
0033227663
-
Regulation About Time-Varying Trajectories: Precision Entry Guidance Illustrated
-
P. Lu, "Regulation About Time-Varying Trajectories: Precision Entry Guidance Illustrated," Journal of Guidance, Control, and Dynamics, vol. 22, no. 6, pp. 784-790, 1999.
-
(1999)
Journal of Guidance, Control, and Dynamics
, vol.22
, Issue.6
, pp. 784-790
-
-
Lu, P.1
-
22
-
-
85088724345
-
Profile-Following Entry Guidance Using Linear Quadratic Regulator Theory
-
AIAA Paper 2002-4457, August
-
G. Dukeman, "Profile-Following Entry Guidance Using Linear Quadratic Regulator Theory," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2002-4457, August 2002.
-
(2002)
AIAA Guidance, Navigation, and Control Conference
-
-
Dukeman, G.1
-
23
-
-
0042266443
-
Automated Method to Compute Orbital Reentry Trajectories with Heating Constraints
-
C. Zimmerman, G. Dukeman, and J. Hanson, "Automated Method to Compute Orbital Reentry Trajectories with Heating Constraints," Journal of Guidance, Control, and Dynamics, vol. 26, no. 4, pp. 523-529, 2003.
-
(2003)
Journal of Guidance, Control, and Dynamics
, vol.26
, Issue.4
, pp. 523-529
-
-
Zimmerman, C.1
Dukeman, G.2
Hanson, J.3
-
24
-
-
85088195092
-
Ascent, Transition, Entry, and Abort Guidance Algorithm Design for the X-33 Vehicle
-
AIAA Paper 1998-4409, August
-
J. M. Hanson, D. J. Coughlin, G. A. Dukeman, J. A. Mulqueen, and J. W. McCarter, "Ascent, Transition, Entry, and Abort Guidance Algorithm Design for the X-33 Vehicle," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 1998-4409, August 1998.
-
(1998)
AIAA Guidance, Navigation, and Control Conference
-
-
Hanson, J.M.1
Coughlin, D.J.2
Dukeman, G.A.3
Mulqueen, J.A.4
McCarter, J.W.5
-
25
-
-
0036494418
-
Dynamic Inversion-Based Adaptive/ Reconfigurable Control of the X-33 on Ascent
-
D. Doman and A. Ngo, "Dynamic Inversion-Based Adaptive/ Reconfigurable Control of the X-33 on Ascent," Journal of Guidance, Control, and Dynamics, vol. 25, no. 2, pp. 275-284, 2002.
-
(2002)
Journal of Guidance, Control, and Dynamics
, vol.25
, Issue.2
, pp. 275-284
-
-
Doman, D.1
Ngo, A.2
-
26
-
-
34047205537
-
Reconfigurable Flight Control Designs with Application to the X-33 Vehicle
-
AIAA Paper 1999-4134, August
-
J. J. Burken, P. Lu, and Z. Wu, "Reconfigurable Flight Control Designs with Application to the X-33 Vehicle," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 1999-4134, August 1999.
-
(1999)
AIAA Guidance, Navigation, and Control Conference
-
-
Burken, J.J.1
Lu, P.2
Wu, Z.3
-
27
-
-
0344898942
-
Limited Authority Adaptive Flight Control for Reusable Launch Vehicles
-
E. N. Johnson and A. J. Calise, "Limited Authority Adaptive Flight Control for Reusable Launch Vehicles," Journal of Guidance, Control, and Dynamics, vol. 26, no. 6, pp. 906-913, 2003.
-
(2003)
Journal of Guidance, Control, and Dynamics
, vol.26
, Issue.6
, pp. 906-913
-
-
Johnson, E.N.1
Calise, A.J.2
-
28
-
-
85086488922
-
Direct Fault Tolerant RLV Attitude Control - A Singular Perturbation Approach
-
AIAA Paper 2002-4778, August
-
J. Zhu, D. Lawrence, J. Fisher, A. Hodel, and P. Lu, "Direct Fault Tolerant RLV Attitude Control - A Singular Perturbation Approach," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2002-4778, August 2002.
-
(2002)
AIAA Guidance, Navigation, and Control Conference
-
-
Zhu, J.1
Lawrence, D.2
Fisher, J.3
Hodel, A.4
Lu, P.5
-
29
-
-
2942750239
-
Improved Trajectory Linearization Flight Controller for Reusable Launch Vehicles
-
AIAA Paper 2004-875, Jan
-
T. Bevacqua, E. Best, A. Huizenga, D. Cooper, and J. Zhu, "Improved Trajectory Linearization Flight Controller for Reusable Launch Vehicles," in 42nd AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2004-875, Jan. 2004.
-
(2004)
42nd AIAA Aerospace Sciences Meeting and Exhibit
-
-
Bevacqua, T.1
Best, E.2
Huizenga, A.3
Cooper, D.4
Zhu, J.5
-
30
-
-
85088181983
-
Reusable Launch Vehicle Attitude Control Using Time-Varying Sliding Modes
-
AIAA Paper 2002-4779, August
-
Y. Shtessel, J. Zhu, and D. Daniels, "Reusable Launch Vehicle Attitude Control Using Time-Varying Sliding Modes," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2002-4779, August 2002.
-
(2002)
AIAA Guidance, Navigation, and Control Conference
-
-
Shtessel, Y.1
Zhu, J.2
Daniels, D.3
-
31
-
-
85088181226
-
Development of a Hybrid Direct-Indirect Adaptive Control System for the X-33
-
AIAA Paper 2000-4156, August
-
D. B. Doman, A. D. Ngo, D. B. Leggett, M. A. Saliers, and M. Pachter, "Development of a Hybrid Direct-Indirect Adaptive Control System for the X-33," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2000-4156, August 2000.
-
(2000)
AIAA Guidance, Navigation, and Control Conference
-
-
Doman, D.B.1
Ngo, A.D.2
Leggett, D.B.3
Saliers, M.A.4
Pachter, M.5
-
32
-
-
84959101023
-
Integration of On-line System Identification and Optimization-based Control Allocation
-
AIAA Paper 1998-4487, August
-
J. M. Buffington, P. Chandler, and M. Pachter,"Integration of On-line System Identification and Optimization-based Control Allocation," in AIAA Guidance, Navigation and Control Conference, AIAA Paper 1998-4487, August 1998.
-
(1998)
AIAA Guidance, Navigation and Control Conference
-
-
Buffington, J.M.1
Chandler, P.2
Pachter, M.3
-
33
-
-
0029192309
-
A Self-Designing Receding Horizon Optimal Flight Controller
-
IEEE, June
-
D. Ward and R. Barron, "A Self-Designing Receding Horizon Optimal Flight Controller," in American Control Conference, pp. 3490-3494, IEEE, June 1995.
-
(1995)
American Control Conference
, pp. 3490-3494
-
-
Ward, D.1
Barron, R.2
-
34
-
-
0032206954
-
Development and Flight Testing of a Parameter Identification Algorithm for Reconfigurable Control
-
D. G. Ward, J. F. Monaco, and M. Bodson, "Development and Flight Testing of a Parameter Identification Algorithm for Reconfigurable Control," Journal of Guidance, Control, and Dynamics, vol. 21, no. 6, pp. 948-956, 1998.
-
(1998)
Journal of Guidance, Control, and Dynamics
, vol.21
, Issue.6
, pp. 948-956
-
-
Ward, D.G.1
Monaco, J.F.2
Bodson, M.3
-
35
-
-
0036494418
-
Dynamic Inversion-Based Adaptive/ Reconfigurable Control of the X-33 on Ascent
-
D. Doman and A. Ngo, "Dynamic Inversion-Based Adaptive/ Reconfigurable Control of the X-33 on Ascent," Journal of Guidance, Control, and Dynamics, vol. 25, no. 2, pp. 275-284, 2002.
-
(2002)
Journal of Guidance, Control, and Dynamics
, vol.25
, Issue.2
, pp. 275-284
-
-
Doman, D.1
Ngo, A.2
-
36
-
-
34147108755
-
The Role of Structural Health Monitoring for Future Air Vehicles
-
AIAA Paper 2006-1952, May
-
M. Derriso and S. Olson, "The Role of Structural Health Monitoring for Future Air Vehicles," in 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference, AIAA Paper 2006-1952, May 2006.
-
(2006)
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference
-
-
Derriso, M.1
Olson, S.2
-
37
-
-
0003817459
-
-
Tech. Rep. VA-WP-TR-1998-3009, AFRL, WPAFB, OH, Aug
-
W. B. Blake, "Missile Datcom User's Manual -1997 FORTRAN 90 Revision," Tech. Rep. VA-WP-TR-1998-3009, AFRL, WPAFB, OH, Aug. 1998.
-
(1998)
Missile Datcom User's Manual -1997 FORTRAN 90 Revision
-
-
Blake, W.B.1
-
38
-
-
29744443771
-
Online Trajectory Generation for Hypersonic Vehicles
-
AIAA Paper 2005-6435, August
-
D. Allwine, J. Fisher, J. Strahler, D. Lawrence, M. Oppenheimer, and D. Doman,"Online Trajectory Generation for Hypersonic Vehicles," in AIAA Guidance, Navigation and Control Conference, AIAA Paper 2005-6435, August 2005.
-
(2005)
AIAA Guidance, Navigation and Control Conference
-
-
Allwine, D.1
Fisher, J.2
Strahler, J.3
Lawrence, D.4
Oppenheimer, M.5
Doman, D.6
-
39
-
-
29744455290
-
Online Adaptive Estimation and Trajectory Reshaping
-
AIAA Paper 2005-6436, August
-
A. Verma, M. Oppenheimer, and D. Doman,"Online Adaptive Estimation and Trajectory Reshaping," in AIAA Guidance, Navigation and Control Conference, AIAA Paper 2005-6436, August 2005.
-
(2005)
AIAA Guidance, Navigation and Control Conference
-
-
Verma, A.1
Oppenheimer, M.2
Doman, D.3
-
40
-
-
39649122494
-
-
J. M. Buffington,Modular Control Law Design for the Innovative Control Effectors (ICE) Tailless Fighter Aircraft Configuration 101-3, Tech. Rep. AFRL-VA-WP-TR-1999, Air Force Research Laboratory, Wright-Patterson A.F.B., OH, 1999, pp 93-94.
-
J. M. Buffington,"Modular Control Law Design for the Innovative Control Effectors (ICE) Tailless Fighter Aircraft Configuration 101-3," Tech. Rep. AFRL-VA-WP-TR-1999, Air Force Research Laboratory, Wright-Patterson A.F.B., OH, 1999, pp 93-94.
-
-
-
-
42
-
-
0027628139
-
Constrained Control Allocation: Three Moment Problem
-
W. Durham, "Constrained Control Allocation: Three Moment Problem," Journal of Guidance, Control and Dynamics, vol. 16, no. 4, pp. 717-725, 1993.
-
(1993)
Journal of Guidance, Control and Dynamics
, vol.16
, Issue.4
, pp. 717-725
-
-
Durham, W.1
-
44
-
-
35948959995
-
A Highly Adaptable Method of Managing Jets and Aerosurfaces for Control of Aerospace Vehicles
-
AIAA Paper 1989-3429, August
-
J. A. Paradiso, "A Highly Adaptable Method of Managing Jets and Aerosurfaces for Control of Aerospace Vehicles," in AIAA Guidance, Navigation and Control Conference, AIAA Paper 1989-3429, August 1989.
-
(1989)
AIAA Guidance, Navigation and Control Conference
-
-
Paradiso, J.A.1
-
45
-
-
85003212370
-
Adaptable Method of Managing Jets and Aerosurfaces for Aerospace Vehicle Control
-
J. A. Paradiso, "Adaptable Method of Managing Jets and Aerosurfaces for Aerospace Vehicle Control," Journal of Guidance, Control and Dynamics, vol. 14, no. 1, pp. 44-50, 1991.
-
(1991)
Journal of Guidance, Control and Dynamics
, vol.14
, Issue.1
, pp. 44-50
-
-
Paradiso, J.A.1
-
46
-
-
85076579473
-
Dynamic Control Allocation Using Constrained Quadratic Programming
-
AIAA Paper 2002-4761, August
-
O. Härkegård,"Dynamic Control Allocation Using Constrained Quadratic Programming," in AIAA Guidance, Navigation and Control Conference, AIAA Paper 2002-4761, August 2002.
-
(2002)
AIAA Guidance, Navigation and Control Conference
-
-
Härkegård, O.1
-
47
-
-
0036641408
-
Evaluation of Optimization Methods for Control Allocation
-
M. Bodson, "Evaluation of Optimization Methods for Control Allocation," Journal of Guidance, Control and Dynamics, vol. 25, no. 4, pp. 703-711, 2002.
-
(2002)
Journal of Guidance, Control and Dynamics
, vol.25
, Issue.4
, pp. 703-711
-
-
Bodson, M.1
-
48
-
-
85088759281
-
Improving Control Allocation Accuracy for Nonlinear Aircraft Dynamics
-
AIAA Paper 2002-4667, August
-
D. B. Doman and M. W. Oppenheimer, "Improving Control Allocation Accuracy for Nonlinear Aircraft Dynamics," in AIAA Guidance, Navigation and Control Conference, AIAA Paper 2002-4667, August 2002.
-
(2002)
AIAA Guidance, Navigation and Control Conference
-
-
Doman, D.B.1
Oppenheimer, M.W.2
-
49
-
-
85085401566
-
Non-linear Control Allocation Using Piecewise Linear Functions
-
AIAA Paper 2003-5357, August
-
M. Bolender and D. B. Doman, "Non-linear Control Allocation Using Piecewise Linear Functions," in AIAA Guidance, Navigation and Control Conference, AIAA Paper 2003-5357, August 2003.
-
(2003)
AIAA Guidance, Navigation and Control Conference
-
-
Bolender, M.1
Doman, D.B.2
-
50
-
-
4944219589
-
Methods for Compensating for Control Allocator and Actuator Interactions
-
M. W. Oppenheimer and D. B. Doman, "Methods for Compensating for Control Allocator and Actuator Interactions," Journal of Guidance, Control, and Dynamics, vol. 27, no. 5, pp. 922-927, 2004.
-
(2004)
Journal of Guidance, Control, and Dynamics
, vol.27
, Issue.5
, pp. 922-927
-
-
Oppenheimer, M.W.1
Doman, D.B.2
-
51
-
-
8744273704
-
Model Predictive Dynamic Control Allocation with Actuator Dynamics
-
Y. Luo, S. Yurkovich, A. Serrani, D. B. Doman, and M. W. Oppenheimer,"Model Predictive Dynamic Control Allocation with Actuator Dynamics," in Proceedings of American Control Conference, 2004.
-
(2004)
Proceedings of American Control Conference
-
-
Luo, Y.1
Yurkovich, S.2
Serrani, A.3
Doman, D.B.4
Oppenheimer, M.W.5
-
52
-
-
8744239033
-
Control Allocation for the X-33 using Existing and Novel Quadratic Programming Techniques
-
A. Simmons and A. Hodel, "Control Allocation for the X-33 using Existing and Novel Quadratic Programming Techniques," in Proceedings of American Control Conference, 2004.
-
(2004)
Proceedings of American Control Conference
-
-
Simmons, A.1
Hodel, A.2
-
53
-
-
85085777346
-
A Six Degree-of-Freedom Adaptive Flight Control Architecture for Trajectory Following
-
AIAA Paper 2002-4776, August
-
E. N. Johnson, A. J. Calise, and E. J. Corban, "A Six Degree-of-Freedom Adaptive Flight Control Architecture for Trajectory Following," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2002-4776, August 2002.
-
(2002)
AIAA Guidance, Navigation, and Control Conference
-
-
Johnson, E.N.1
Calise, A.J.2
Corban, E.J.3
-
54
-
-
33845762382
-
Optimal Non-linear Feedback Guidance for Reentry Vehicles
-
AIAA Paper 2006-6074, Aug
-
K. Bollino, I. Ross, and D. B. Doman, "Optimal Non-linear Feedback Guidance for Reentry Vehicles," in AIAA Guidance, Navigation and Control Conference, AIAA Paper 2006-6074, Aug. 2006.
-
(2006)
AIAA Guidance, Navigation and Control Conference
-
-
Bollino, K.1
Ross, I.2
Doman, D.B.3
-
55
-
-
33845760933
-
Optimal Guidance Command Generation and Tracking for Reusable Launch Vehicle Reentry
-
AIAA Paper 2006-6691, Aug
-
K. Bollino, M. Oppenheimer, and D. Doman, "Optimal Guidance Command Generation and Tracking for Reusable Launch Vehicle Reentry," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2006-6691, Aug. 2006.
-
(2006)
AIAA Guidance, Navigation, and Control Conference
-
-
Bollino, K.1
Oppenheimer, M.2
Doman, D.3
-
56
-
-
39649095502
-
Validation & Verification of Intelligent and Adaptive Control Systems
-
IEEEAC Paper 1439
-
V. Crum, J. Buffington, G. Tallant, B. Krogh, C. Plaisted, R. Prasanth, P. Bose, and T. Johnson, "Validation & Verification of Intelligent and Adaptive Control Systems," in Proceedings of IEEE Aerospace Conference, IEEEAC Paper 1439.
-
Proceedings of IEEE Aerospace Conference
-
-
Crum, V.1
Buffington, J.2
Tallant, G.3
Krogh, B.4
Plaisted, C.5
Prasanth, R.6
Bose, P.7
Johnson, T.8
-
57
-
-
84983185773
-
Determination of X-36 Stability Margins Using Real-Time Frequency Response Techniques
-
AIAA Paper 98-4154, August
-
D. L. Balough, "Determination of X-36 Stability Margins Using Real-Time Frequency Response Techniques," in AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 98-4154, August 1998.
-
(1998)
AIAA Atmospheric Flight Mechanics Conference
-
-
Balough, D.L.1
-
59
-
-
0002573820
-
The Simplex Architecture for Safe On-Line Control System Upgrades
-
June
-
D.Seto, B. Krogh, L. Sha, and A. Chutinan, "The Simplex Architecture for Safe On-Line Control System Upgrades," in Proceedings of the American Control Conference, June 1998.
-
(1998)
Proceedings of the American Control Conference
-
-
Seto, D.1
Krogh, B.2
Sha, L.3
Chutinan, A.4
-
60
-
-
33845792052
-
Are Phase and Time-delay Margins Always Adversely Affected by High-Gain?
-
AIAA, August
-
C. Cao, V. Patel, C. Reddy, N. Hovakimyan, E. Lavretsky, and K. Wise, "Are Phase and Time-delay Margins Always Adversely Affected by High-Gain?," in AIAA Guidance, Navigation, and Control Conference, AIAA, August 2006.
-
(2006)
AIAA Guidance, Navigation, and Control Conference
-
-
Cao, C.1
Patel, V.2
Reddy, C.3
Hovakimyan, N.4
Lavretsky, E.5
Wise, K.6
-
61
-
-
33846877867
-
In-Flight TAEM/Final Approach Trajectory Generation for Reusable Launch Vehicles
-
AIAA Paper 2005-7114, August
-
J. Hull, N. Gandhi, and J. D. Schierman, "In-Flight TAEM/Final Approach Trajectory Generation for Reusable Launch Vehicles," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2005-7114, August 2005.
-
(2005)
AIAA Guidance, Navigation, and Control Conference
-
-
Hull, J.1
Gandhi, N.2
Schierman, J.D.3
-
62
-
-
29744459512
-
Optimal Trajectory Reconfiguration and Retargeting for a Reusable Launch Vehicle
-
AIAA Paper 2005-6148, August
-
P. Shaffer, I. Ross, M. Oppenheimer, and D. Doman, "Optimal Trajectory Reconfiguration and Retargeting for a Reusable Launch Vehicle," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2005-6148, August 2005.
-
(2005)
AIAA Guidance, Navigation, and Control Conference
-
-
Shaffer, P.1
Ross, I.2
Oppenheimer, M.3
Doman, D.4
-
63
-
-
1842554869
-
New, Fast Numerical Method for Solving Two-Point Boundary-Value Problems
-
R. W. Holsapple, R. Venkataraman, and D. Doman, "New, Fast Numerical Method for Solving Two-Point Boundary-Value Problems," Journal of Guidance, Control, and Dynamics, vol. 27, no. 2, pp. 301-304, 2004.
-
(2004)
Journal of Guidance, Control, and Dynamics
, vol.27
, Issue.2
, pp. 301-304
-
-
Holsapple, R.W.1
Venkataraman, R.2
Doman, D.3
-
64
-
-
19644367556
-
A Direct Method for Approach and Landing Trajectory Reshaping with Failure Effect Estimation
-
AIAA Paper 2004-4772, August
-
F. Fahroo and D. Doman, "A Direct Method for Approach and Landing Trajectory Reshaping with Failure Effect Estimation," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2004-4772, August 2004.
-
(2004)
AIAA Guidance, Navigation, and Control Conference
-
-
Fahroo, F.1
Doman, D.2
-
65
-
-
34250699512
-
X-43 Scramjet Power Breaks the Hypersonic Barrier: Dryden Lectureship in Research for 2006
-
AIAA Paper 2006-0001, January
-
C. McClinton, "X-43 Scramjet Power Breaks the Hypersonic Barrier: Dryden Lectureship in Research for 2006," in 44th AIAA Aerospace Sciences Meeting, AIAA Paper 2006-0001, January 2006.
-
(2006)
44th AIAA Aerospace Sciences Meeting
-
-
McClinton, C.1
-
66
-
-
0028546482
-
Analytical Aeropropulsive/Aeroelastic Hypersonic-Vehicle Model with Dynamic Analysis
-
Nov-Dec
-
F. Chavez and D. Schmidt, "Analytical Aeropropulsive/Aeroelastic Hypersonic-Vehicle Model with Dynamic Analysis," Journal of Guidance, Control, and Dynamics, vol. 17, pp. 1308- 1319, Nov-Dec 1994.
-
(1994)
Journal of Guidance, Control, and Dynamics
, vol.17
, pp. 1308-1319
-
-
Chavez, F.1
Schmidt, D.2
-
67
-
-
84888835872
-
A Nonlinear Longitudinal Dynamical Model of an Air-breathing Hypersonic Vehicle
-
to appear
-
M. Bolender and D. Doman, "A Nonlinear Longitudinal Dynamical Model of an Air-breathing Hypersonic Vehicle," Journal of Spacecraft and Rockets. to appear.
-
Journal of Spacecraft and Rockets
-
-
Bolender, M.1
Doman, D.2
-
68
-
-
33751409313
-
Modelling Unsteady Heating Effects on the Structural Dynamic of a Hypersonic Vehicle
-
AIAA Paper 2006-6646, August
-
M. A. Bolender and D. B. Doman, "Modelling Unsteady Heating Effects on the Structural Dynamic of a Hypersonic Vehicle," in AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 2006-6646, August 2006.
-
(2006)
AIAA Atmospheric Flight Mechanics Conference
-
-
Bolender, M.A.1
Doman, D.B.2
-
69
-
-
33751423005
-
Flexible Mode Analysis of a Hypersonic Vehicle
-
AIAA Paper 2006-6647, Aug
-
T. Williams, M. A. Bolender, D. B. Doman, and O. Morataya, "Flexible Mode Analysis of a Hypersonic Vehicle," in AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 2006-6647, Aug. 2006.
-
(2006)
AIAA Atmospheric Flight Mechanics Conference
-
-
Williams, T.1
Bolender, M.A.2
Doman, D.B.3
Morataya, O.4
-
71
-
-
0029343262
-
Stability Derivatives for a Hypersonic Caret-Wing Waverider
-
C. Tarpley and M. Lewis, "Stability Derivatives for a Hypersonic Caret-Wing Waverider," Journal of Aircraft, vol. 32, no. 4, pp. 795-803, 1995.
-
(1995)
Journal of Aircraft
, vol.32
, Issue.4
, pp. 795-803
-
-
Tarpley, C.1
Lewis, M.2
-
73
-
-
33845789624
-
Flight Path Angle Dynamics of Air-breathing Hypersonic Vehicles
-
AIAA Paper 2006-6692, August
-
M. Bolender and D. Doman, "Flight Path Angle Dynamics of Air-breathing Hypersonic Vehicles," in AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2006-6692, August 2006.
-
(2006)
AIAA Guidance, Navigation, and Control Conference
-
-
Bolender, M.1
Doman, D.2
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