A hybrid fault-tolerant scheme for flight control applications

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Bošković, Jovan D ^a   Mehra, Raman K ^a  

^a SCIENTIFIC SYSTEMS COMPANY INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894487231     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. F. Ahmed-Zaid, P. loannou, K. Gousman and R. Rooney,'Accommodation of Failures in the F-16 Aircraft using Adaptive Control', IEEE Control Systems Magazine, Vol. 11, No. 1, pp. 73-78, January 1991.
2. M. Bodson and J. Groszkiewicz,'Multivariable Adaptive Algorithms for Reconfigurable Flight Control', IEEE Transactions on Control Systems Technology, Vol. 5, No. 2, pp. 217-229, March 1997.
3. Boeing Phantom Works,'Reconfigurable Systems for Tailless Fighter Aircraft-RESTORE', Scientific and Technical Reports, St. Louis, Missouri, May 1998.
4. J. D. Bošković, S.-M. Li and R. K. Mehra,'Evaluation of the Properties of a Multiple-Model Reconfigurable Flight Controller on a 6 DOF Simulation', Proc. AIAA Guidance, Navigation and Control Conference, Denver, CO, August 2000.
5. J. D. Bošković, S.-M. Li, and R. K. Mehra,'Design Assistant and Software Tools for System Identification and Adaptive Fault-Tolerant Control of Fighter Aircraft', Final Report for the Navy Phase ISBIR, May 2000.
6. J. D. Bošković, E. S.-M. Li and R. K. Mehra,'Research on System Identification and FDI for Reconfigurable Flight Control System', Final Report, Task 14, Boeing/NASA Langley, Scientific Systems Company, Inc., 1999.
7. J. D. Bošković and R. K. Mehra,'Intelligent Adaptive Control of a Tailless Advanced Fighter Aircraft (TAFA) in the Presence of Wing Damage', in Proceedings of the AIAA Guidance, Navigation and Control Conference, Vol. 1, pp. 455-465, Portland, OR, August 1999.
8. J. D. Bošković and R. K. Mehra,'Stable Multiple Model Adaptive Flight Control for Accommodation of a Large Class of Control Effector Failures', in Proceedings of the 1999 American Control Conference, pp. 1920-1924, San Diego, CA, June 1999.
9. J. D. Bošković and R. K. Mehra,'A Multiple Model-based Reconfigurable Flight Control System Design', in Proceeding of the 1998 Conference on Decision and Control, Tampa, FL, December 1998.
10. J. D. Bošković, S.-H. Yu, and R. K. Mehra,'Stable Adaptive Fault-Tolerant Control of Overactuated Aircraft using Multiple Models, Switching and Tuning', in Proceedings of the 1998 AIAA Guidance, Navigation and Control Conference, Vol. 1, pp. 739-749, Boston, MA, August 10-12, 1998.
11. J. D. Bošković, S.-H. Yu, and R. K. Mehra,'A Stable Scheme for Automatic Control Reconfiguration in the Presence of Actuator Failures', in Proceedings of the 1998 American Control Conference, Vol. 4, pp. 2455-2459, Philadelphia, PA, June 24-26, 1998.
12. J. Brinker and K. Wise, 'Reconfigurable Flight Control of a Tailless Advanced Fighter Aircraft, in Proceedings of the 1998 AIAA Guidance, Navigation and Control Conference, Vol. 1, pp. 75-87, Boston, MA, August 10-12, 1998.
13. A. Calise, S. Lee and M. Sharma,'Direct Adaptive Reconfigurable Control of a Tailless Fighter Aircraft', in Proceedings of the 1998 AIAA Guidance, Navigation and Control Conference, Vol. 1, pp. 88-97, Boston, MA, August 10-12, 1998.
14. P. Chandler, M. Pachter and M. Mears,'System Identification for Adaptive and Reconfigurable Control', Journal of Guidance, Control & Dynamics, Vol. 18, No. 3, pp. 516-524, May-June 1995.
15. K. S. Narendra and A. M. Annaswamy (1988), Stable Adaptive Systems, Prentice Hall Inc., Englewood Cliffs, New Jersey.
16. K. S. Narendra and J. Balakrishnan, ' Adaptive Control using Multiple Models', IEEE Transactions on Automatic Control, Vol. 42, No. 2, pp. 171-187, February 1997.
17. M. Pachter and P. R. Chandler,'Challenges of Autonomous Control', IEEE Control Systems Magazine, pp. 92-97, Vol. 18, No. 4, August 1998.
18. RESTORE Final Briefing, WPAFB, OH, August 1999