-
1
-
-
0041628554
-
Aircraft accident report - United airlines flight 232
-
National Transportation Safety Board Washington, DC
-
National Transportation Safety Board, "Aircraft Accident Report - United Airlines Flight 232," Report NTSB/AAR-90/06, Washington, DC, 1990.
-
(1990)
Report NTSB/AAR-90/06
-
-
-
2
-
-
78651084725
-
Flying with no flight controls: Handling qualities analyses of the baghdad event
-
AIAA-2005-5907, AIAA, Washington, DC
-
Lemaignan, B., "Flying with no Flight Controls: Handling Qualities Analyses of the Baghdad Event," AIAA Atmospheric Flight Mechanics Conference and Exhibit, AIAA-2005-5907, AIAA, Washington, DC, 2008.
-
(2008)
AIAA Atmospheric Flight Mechanics Conference and Exhibit
-
-
Lemaignan, B.1
-
3
-
-
84959082074
-
Nonlinear simulation analysis of a tailless advanced fighter aircraft reconfigurable flight control law
-
AIAA-99-4040, AIAA, Washington, DC
-
Brinker, S.J. and Wise, K.A. "Nonlinear simulation analysis of a tailless advanced fighter aircraft reconfigurable flight control law,". AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA-99-4040, AIAA, Washington, DC, 1999.
-
(1999)
AIAA Guidance, Navigation and Control Conference and Exhibit
-
-
Brinker, S.J.1
Wise, K.A.2
-
4
-
-
0035440105
-
Development of a reconfigurable flight control law for the x-36 tailless fighter aircraft
-
Calise, A.J., Lee, S. and Sharma, M. "Development of a reconfigurable flight control law for the x-36 tailless fighter aircraft," AIAA Journal of Guidance, Control and Dynamics, 24(5):896-902, 2001.
-
(2001)
AIAA Journal of Guidance, Control and Dynamics
, vol.24
, Issue.5
, pp. 896-902
-
-
Calise, A.J.1
Lee, S.2
Sharma, M.3
-
5
-
-
0013016031
-
Self-repairing flight control systems, volume i: Flight test evaluation on an f-15 aircraft
-
Corvin, J.H., Havern, W.H., Hoy, S.E., Norat, K.F., Urnes, J.M. and Wells E.A., "Self-repairing flight control systems, volume i: Flight test evaluation on an f-15 aircraft," Final Report WL-TR-91-3025, 1991.
-
(1991)
Final Report WL-TR-91-3025
-
-
Corvin, J.H.1
Havern, W.H.2
Hoy, S.E.3
Norat, K.F.4
Urnes, J.M.5
Wells, E.A.6
-
7
-
-
0036055812
-
Enhanced NDI strategies for reconfigurable flight control
-
Anchorage, AK
-
Ostroff, A.J. and Bacon, B.J., "Enhanced NDI strategies for reconfigurable flight control," American Control Conference, Anchorage, AK, 2002.
-
(2002)
American Control Conference
-
-
Ostroff, A.J.1
Bacon, B.J.2
-
8
-
-
33846539049
-
A simulation benchmark for integrated fault tolerant flight control evaluation
-
AIAA-2006-6471, AIAA, Washington, DC
-
Smaili, M.H., Breeman, J., Lombaerts, T.J.J., and Joosten, D.A., "A Simulation Benchmark for Integrated Fault Tolerant Flight Control Evaluation," AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA-2006-6471, AIAA, Washington, DC, 2006.
-
(2006)
AIAA Modeling and Simulation Technologies Conference and Exhibit
-
-
Smaili, M.H.1
Breeman, J.2
Lombaerts, T.J.J.3
Joosten, D.A.4
-
9
-
-
85085778169
-
Using the SIMONA research simulator for human-machine interaction research
-
AIAA-2003-5525, AIAA, Washington, DC
-
Stroosma, O., Van Paassen, M.M., and Mulder, M., "Using the SIMONA Research Simulator for Human-Machine Interaction Research," AIAA Modeling and Simulation Technologies Conference, AIAA-2003-5525, AIAA, Washington, DC, 2003.
-
(2003)
AIAA Modeling and Simulation Technologies Conference
-
-
Stroosma, O.1
Van Paassen, M.M.2
Mulder, M.3
-
10
-
-
78651060567
-
The simulation of a large transport aircraft volume I: Mathematical model
-
Hanke, C.R., "The Simulation of a Large Transport Aircraft Volume I: Mathematical Model," NASA CR-1756, 1971.
-
(1971)
NASA CR-1756
-
-
Hanke, C.R.1
-
11
-
-
1842420807
-
A boeing 747-100/200 aircraft fault tolerant and fault diagnostic benchmark
-
Minneapolis, MN
-
Marcos, A., and Balas, G.J., "A Boeing 747-100/200 aircraft fault tolerant and fault diagnostic benchmark," Technical Report AEM-UoM-2003-1, University of Minnesota, Minneapolis, MN, 2003.
-
(2003)
Technical Report AEM-UoM-2003-1, University of Minnesota
-
-
Marcos, A.1
Balas, G.J.2
-
12
-
-
78651071804
-
-
Nederlands Aviation Safety Board Report 92-11, Hoofddorp, The Netherlands
-
Nederlands Aviation Safety Board, "Aircraft Accident Report El Al Flight 1862," Report 92-11, Hoofddorp, The Netherlands, 1994.
-
(1994)
Aircraft Accident Report el Al Flight 1862
-
-
-
13
-
-
78651063647
-
Flight data reconstruction and simulation of EL AL flight 1862
-
AIAA-2000-4586, AIAA, Washington, DC
-
Smaili M.H and Mulder J.A., "Flight data reconstruction and simulation of EL AL Flight 1862," AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA-2000-4586, AIAA, Washington, DC, 2000.
-
(2000)
AIAA Modeling and Simulation Technologies Conference and Exhibit
-
-
Smaili, M.H.1
Mulder, J.A.2
-
14
-
-
78651060065
-
Piloted sliding mode FTC simulator evaluation for the EL AL flight 1862 incident
-
AIAA-2008-7157, AIAA, Washington, DC
-
Alwi, H., Edwards, C., Stroosma, O. and Mulder, J.A., "Piloted Sliding Mode FTC Simulator Evaluation for the EL AL Flight 1862 Incident," AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA-2008-7157, AIAA, Washington, DC, 2008.
-
(2008)
AIAA Guidance, Navigation and Control Conference and Exhibit
-
-
Alwi, H.1
Edwards, C.2
Stroosma, O.3
Mulder, J.A.4
-
15
-
-
43649084389
-
Development of an active fault-tolerant flight control strategy
-
Cieslak, J., Henry, D. Zolghadri, A. and Goupil, P., "Development of an Active Fault-Tolerant Flight Control Strategy," AIAA Journal of Guidance, Control, and Dynamics, Vol. 31, No. 1, 2008, pp. 135-147.
-
(2008)
AIAA Journal of Guidance, Control, and Dynamics
, vol.31
, Issue.1
, pp. 135-147
-
-
Cieslak, J.1
Henry, D.2
Zolghadri, A.3
Goupil, P.4
-
16
-
-
77951686297
-
-
Ph.D. Dissertation, Delft Center for Systems and Control, Delft University of Technology, Delft, The Netherlands
-
Hallouzi, R., "Multiple-Model Based Diagnosis for Adaptive Fault-Tolerant Control," Ph.D. Dissertation, Delft Center for Systems and Control, Delft University of Technology, Delft, The Netherlands, 2008.
-
(2008)
Multiple-Model Based Diagnosis for Adaptive Fault-Tolerant Control
-
-
Hallouzi, R.1
-
17
-
-
77953753553
-
Flight control reconfiguration based on online physical model identification and nonlinear dynamic inversion
-
AIAA-2008-7435, AIAA, Washington, DC
-
Lombaerts, T.J.J., Huisman, H., Chu, Q.P., Mulder, J.A., and Joosten, D.A., "Flight Control Reconfiguration based on Online Physical Model Identification and Nonlinear Dynamic Inversion," AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA-2008-7435, AIAA, Washington, DC, 2008.
-
(2008)
AIAA Guidance, Navigation and Control Conference and Exhibit
-
-
Lombaerts, T.J.J.1
Huisman, H.2
Chu, Q.P.3
Mulder, J.A.4
Joosten, D.A.5
-
18
-
-
85087604414
-
DUECA - Data-driven activation in distributed realtime computation
-
AIAA 2000-4503, AIAA, Washington, DC
-
Van Paassen, M.M., Stroosma, O., Delatour, J., "DUECA - Data-driven Activation in Distributed Realtime Computation," AIAA Modeling and Simulation Technologies Conference, AIAA 2000-4503, AIAA, Washington, DC, 2000.
-
(2000)
AIAA Modeling and Simulation Technologies Conference
-
-
Van Paassen, M.M.1
Stroosma, O.2
Delatour, J.3
-
19
-
-
0006453401
-
The use of pilot rating in the evaluation of aircraft handling qualities
-
Cooper, G.E., and Harper, R.P. Jr., "The Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities," NASA TN D-5153, 1969.
-
(1969)
NASA TN D-5153
-
-
Cooper, G.E.1
Harper Jr., R.P.2
|