Fault tolerance through direct adaptive control using neural networks

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006

Volumn 6, Issue , 2006, Pages 3584-3603

  Johnson, Eric N ^a,b,c   Calise, Anthony J ^a,c   Turbe, Michael A ^a,c  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b Department of Avionics Integration ^*  (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE ALGORITHMS; ADAPTIVE CONTROL SYSTEMS; MATHEMATICAL MODELS; NEURAL NETWORKS; PARAMETER ESTIMATION; VEHICLES;

DYNAMICS MODELS; FAULT TOLERANT CONTROL; NEURAL NETWORK ADAPTATION; REUSABLE LAUNCH VEHICLES;

FAULT TOLERANT COMPUTER SYSTEMS;

EID: 33845788748     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-6553     Document Type: Conference Paper

References (18)

1. Nardi, F., Rysdyk, R. T., and Calise, A. J., "Neural Network Based Adaptive Control of a Thrust Vectored Ducted Fan," AIAA 99-3996, 1999, pp. 1-2.
2. Johnson, E. N. and Kannan, S. K., "Adaptive Trajectory Control for Autonomous Helicopters," Journal of Guidance, Control, and Dynamics, Vol. 28, No. 3, 2005, pp. 524-538.
3. Johnson, E. N., "Limited Authority Adaptive Flight Control," Ph.D. Thesis, Georgia Institute of Technology, 2000.
4. Idan, M., Johnson, M., Calise, A. J., "Hierarchical Approach to Adaptive Control for Improved Flight Safety," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 6, 2002, pp. 1012-1020.
5. Brinker, J. S. and Wise, K. A., "Flight Testing of Reconfigurable Control Law on the X-36 Tailless Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 903-909.
6. Calise, A. J., Lee, S., and Sharma, M., "Development of a Reconfigurable Flight Control Law for Tailless Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 896-902.
7. Hanson, J. M., Coughlin, D. J., Dukeman, G. A., Mulqueen, J. A., and McCarter, J. W., "Ascent, Transition, Entry, and Abort Guidance Algorithm Design for the X-33 Vehicle," AIAA Guidance, Navigation, and Control Conf., AIAA 98-4409, Aug. 1998.
8. Johnson, M. D., Calise, A. J., and Johnson, E. N., "Evaluation of an Adaptive Method for Launch Vehicle Flight Control," AIAA Guidance, Navigation, and Control Conf., AIAA 2003-5789, Aug. 2003.
9. Johnson, M. D., Calise, A. J., and Johnson, E. N., "Further Evaluation of an Adaptive Method for Launch Vehicle Flight Control," AIAA Guidance, Navigation, and Control Conf., AIAA 2004-5016, Aug. 2004.
10. Hall, C. E., Gallaher, M. W., and Hendrix, N. D., "X-33 Attitude Control System Design for Ascent, Transition, and Entry Flight Regimes," AIAA Guidance, Navigation, and Control Conf., AIAA 1998-4411, Aug. 1998.
11. Johnson, E. N. and Schrage, D. P., "System Integration and Operation of a Research Unmanned Aerial Vehicle," Journal of Aerospace Computing, Information, and Communication, Vol. 1, No. 1, 2004, pp. 8-10.
12. Christophersen, H. B., Pickell, R. W., Neidhoefer, J. C., Koller, A. A., Kannan, S. K., and Johnson, E. N., "A Compact Guidance, Navigation, and Control System for Unmanned Aerial Vehicles," Journal of Aerospace Computing, Information, and Communication, Vol. 3, No. 5, 2006, pp. 187-213.
13. Johnson, E. N. and Turbe, M. A., "Modeling, Control, and Flight Testing of a Small Ducted Fan Aircraft," AIAA Guidance, Navigation, and Control Conf., AIAA 2005-6281, Aug. 2005.
14. Brinker, J.S. and Wise, K.A., "Reconfigurable Flight Control for a Tailless Advanced Fighter Aircraft," AIAA Guidance, Navigation, and Control Conf, AIAA-98-4107, Aug. 1998.
15. Snell, S. A., Enns, D. F., and Garrard Jr., W. L., "Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp. 976-984.
16. 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.
17. Drozeski, G. R., Saha, B., Vachtsevanos, G. J., "A Fault Detection and Reconfigurable Control Architecture for Unmanned Aerial Vehicles," IEEE Aerospace Conf, IEEEAC # 1225, Mar. 2005.
18. Calise, A. J., Lee, S., and Sharma, M., "Direct Adaptive Reconfigurable Control of a Tailless Fighter Aircraft," AIAA Guidance, Navigation, and Control Conf, AIAA 98-4108, Aug. 1998.