Year |
Citation |
Score |
2002 |
Nelson MD, Durham WC. A comparison of two methods used to deal with saturation of multiple, redundant aircraft control effectors Aiaa Atmospheric Flight Mechanics Conference and Exhibit. |
0.339 |
|
2001 |
Durham WC. Computationally efficient control allocation Journal of Guidance, Control, and Dynamics. 24: 519-524. DOI: 10.2514/2.4741 |
0.476 |
|
1999 |
Durham WC. Efficient, Near-Optimal Control Allocation Journal of Guidance, Control, and Dynamics. 22: 369-372. DOI: 10.2514/2.4390 |
0.398 |
|
1999 |
Scalera KR, Durham WC. A comparison of control allocation methods for the F-15 active research aircraft utilizing real-time piloted simulations 1999 Guidance, Navigation, and Control Conference and Exhibit. 1653-1663. |
0.475 |
|
1998 |
Durham WC, Leedy JQ. Real-time evaluation of control allocation with rate limiting 23rd Atmospheric Flight Mechanics Conference. 752-761. |
0.483 |
|
1998 |
Glaze M, Durham WC. Design and implementation of a control allocation Toolbox for MATLAB® v. 5.0 1998 Guidance, Navigation, and Control Conference and Exhibit. 1544-1553. |
0.415 |
|
1997 |
Durham WC, Bolling JG, Bordignon KA. Minimum drag control allocation Journal of Guidance, Control, and Dynamics. 20: 190-193. DOI: 10.2514/2.4018 |
0.561 |
|
1997 |
Kocurek JN, Durham WC. Dynamic inversion and model-following flight control: A comparison of performance robustness 22nd Atmospheric Flight Mechanics Conference. 1-16. |
0.349 |
|
1997 |
Bolling JG, Durham WC. Control allocation with adaptive failure control 22nd Atmospheric Flight Mechanics Conference. 719-723. |
0.332 |
|
1996 |
Lutze FH, Durham WC, Mason WH. Unified development of lateral-directional departure criteria Journal of Guidance, Control, and Dynamics. 19: 489-493. DOI: 10.2514/3.21644 |
0.399 |
|
1996 |
Durham WC, Bordignon KA. Multiple control effector rate limiting Journal of Guidance, Control, and Dynamics. 19: 30-37. DOI: 10.2514/3.21576 |
0.398 |
|
1996 |
Durham WC. Dynamic inversion and model-following control 1996 Guidance, Navigation, and Control Conference and Exhibit. 1-9. |
0.389 |
|
1995 |
Durham WC. Control Stick Logic in High-Angle-of-Attack Maneuvering Journal of Guidance Control and Dynamics. 18: 1092-1097. DOI: 10.2514/3.21509 |
0.501 |
|
1995 |
Bordingnon KA, Durham WC. Closed-form solutions to constrained control allocation problem Journal of Guidance Control and Dynamics. 18: 1000-1007. DOI: 10.2514/3.21497 |
0.567 |
|
1995 |
Bordignon KA, Durham WC. Null-space augmented solutions to constrained control allocation problems 1995 Guidance, Navigation, and Control Conference. 328-333. |
0.554 |
|
1994 |
Durham WC. Attainable moments for the constrained control allocation problem Journal of Guidance Control and Dynamics. 17: 1371-1373. DOI: 10.2514/3.21360 |
0.508 |
|
1994 |
Durham WC, Lutze FH, Mason W. Kinematics and aerodynamics of the velocity vector roll Journal of Guidance Control and Dynamics. 17: 1228-1233. DOI: 10.2514/3.21337 |
0.307 |
|
1994 |
Durham WC, Lutze FH, Barlas MR, Munro BC. Nonlinear model-following control application to airplane control Journal of Guidance Control and Dynamics. 17: 570-577. DOI: 10.2514/3.21235 |
0.496 |
|
1994 |
Durham WC. Constrained control allocation - Three-moment problem Journal of Guidance Control and Dynamics. 17: 330-336. DOI: 10.2514/3.21201 |
0.584 |
|
1993 |
Durham WC. Constrained Control Allocation Journal of Guidance Control and Dynamics. 16: 717-725. DOI: 10.2514/3.21072 |
0.584 |
|
1991 |
Durham WC, Lutze FH. Perfect explicit model-following control solution to imperfect model-following control problems Journal of Guidance Control and Dynamics. 14: 391-397. DOI: 10.2514/3.20651 |
0.419 |
|
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