Theoretically verifiable stability margins for an adaptive controller

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

Volumn 5, Issue , 2006, Pages 2821-2834

  Dydek, Zachary T ^a,c   Jain, Himani ^a,c   Jinho, Jang ^a,c   Annaswamy, Anuradha M ^a,c   Lavretsky, Eugene ^b  

^a MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

^b BOEING COMPANY   (United States)

^c Mechanical Engineering Department   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE FLIGHT CONTROL SYSTEM (AFCS); LINEAR MATRIX INEQUALITIES; REDUCED LINEAR ASYMPTOTIC SYSTEM (RLAS);

AIRCRAFT MODELS; ASYMPTOTIC STABILITY; COMPUTER SIMULATION; FEEDBACK; FLIGHT DYNAMICS; OPTIMIZATION; PARAMETER ESTIMATION; ROBUSTNESS (CONTROL SYSTEMS);

ADAPTIVE CONTROL SYSTEMS;

EID: 33845780120     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. Narendra, K. S., and Annaswamy, A. M., Stable Adaptive Systems, Prentice-Hall, Englewood Cliffs, NJ, 1989.
2. Slotine, J. J. E., and Li, W., Applied Nonlinear Control, Prentice Hall, Englewood Cliffs, NJ, 1991.
3. Wohletz, J. M., Paduano, J. D., Annaswamy, A. M., "Retrofit Systems for Reconfiguration in Civil Aviation," Proc. AIAA Guidance, Navigation, and Control Conf., Portland, OR, Aug. 1999, pp. 995-1005.
4. Bodson, M., and Groszkiewicz, J. E., "Multivariable Adaptive Algorithms for Reconfigurable Flight Control," IEEE Transactions on Control Systems Technology, Vol. 5, No. 2, Mar. 1997, pp. 217-229.
5. Kim, K. S., Lee, K. J., and Kim, Y., "Model Following Reconfigurable Flight Control System Design Using Direct Adaptive Scheme,"Proc. AIAA Guidance, Navigation, and Control Conf., Monterey CA, Aug. 5-8, 2002.
6. Tao, G., Joshi, S. M., and Ma, X., "Adaptive State Feedback and Tracking Control of Systems with Actuator Failures," IEEE Transaction on Automatic Control, Vol. 46, No. 1, Jan. 2001, pp. 78-95.
7. Schwager, M., Jain, H., Annaswamy, A.M., and Lavretsky, E., "Towards Verifiable Adaptive Flight Control for Safety Critical Applications,"Proc. AIAA Guidance, Navigation, and Control Conf., San Francisco CA, Aug.l5-18, 2005.
8. Direct Adaptive Control Design using RBF NNs, Eugene Lavretsky. February 13, 2003.
9. Pomet, J.B., Praly, L., Adaptive Nonlinear Regulation: Estimation from Lyapunov Equation. IEEE Transactions on Automatic Control. 37(6): 729-740, 1992.
10. nd IEEE Conference on Decision and Control, Maui Miami, Dec., 2003.
11. Huang, C.-H., Ioannou, J. M., and Safonov, M. G., "Design of Strictly Positive Real Systems Using Constant Output Feedback," IEEE Transactions on Automatic Control, Vol. 44, No. 3, March 1999.
12. Lavretsky, E., and Wise, K., "Adaptive Flight for Manned/Unmanned Military Aircraft," Proc. American Control Conf., 2005.
13. MATLAB optimal control tool box.
14. Sharma, M., et al., "Intelligent Control of Unmanned Air Vehicles", Final Technical Report, AFRL, pp. 134-144, 2004.
15. Hollemari, Euclid C., "Summary of High-Altitude and Entry Flight Control Experience with the X-15 Airplane", NASA TN D-3386, April 1966.
16. Staff of the Flight Research Center, "Experience with the X-15 Adaptive Flight Control System", NASA TN D-6208, March 1971.
17. Karason, S., and Annaswamy, A. M., "Adaptive Control in the Presence of Input Constraints," IEEE Transactions on Automatic Control, vol. 39, pp. 2325-2330, 1994.