A novel approach to reconfigurable control systems design

1995 Guidance, Navigation, and Control Conference

Volumn , Issue , 1995, Pages 1-8

  Dhayagude, Nitin ^a   Gao, Zhiqiang ^a  

^a CLEVELAND STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEMS; FLIGHT CONTROL SYSTEMS; LONGITUDINAL CONTROL; RECONFIGURABLE HARDWARE; SYSTEMS ANALYSIS;

DESIGN APPROACHES; DESIGN PROCEDURE; LINEAR MODELING; PERFECT MODEL; RECONFIGURABLE CONTROL SYSTEMS; SYSTEM CONFIGURATIONS; TRACKING ERRORS; TRACKING PERFORMANCE;

DESIGN;

EID: 7244228925     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Caglayan, A. K., Allen, S. ML, and Wehmuller, K., “Evaluation of a second generation reconfiguration strategy for aircraft flight control systems subjected to actuator failure surface damage”, Proceedings of the 1988 IEEE National Aerospace and Electronics Conference, 520-529.
2. Chan, Y. T., “Perfect model following with a real model”, Proceedings of the Joint American Control Conference, 1973,287-293.
3. Dhayagude, N. J., “Linear model following design approach and stability robustness in reconfigurable control systems”, M. S. Thesis, Cleveland State University, 1993.
4. Erzberger, H., “Analysis and design of model following control systems by state-space techniques”, Proceedings of Joint Automatic Control Conference, 1968,572-581.
5. Gao, Z., and Antsaklis, P. J., “Stability of the pseudoinverse method for reconfigurable control systems”, International Journal of Control, 1991, vol. 53, no. 3, 717-729.
6. Gao, Z., and Antsaklis, P. J., “Reconfigurable control systems design via perfect model following”, International Journal of Control, 1992, vol. 56,783-798.
7. Handelman, D. A., and Stengel, R. F., “Combining expert system and analytic redundancy concepts for fault tolerance flight control”, Journal of Guidance, Control and Dynamics, 1989,12,39-45.
8. Huang, C. Y., and Stengel, R. F., “Restructurable control using proportional-integral implicit model following”, Journal of Guidance, Dynamics and Control, 1990, 13, 303-339.
9. Jiang Jin, “Design of reconfigurable control systems design using eigenstructure assignments”, International Journal of Control, 1994, vol. 59, no. 2,395-410.
10. Landau, Y. D., Adaptive Control: the Model reference Approach, Marcel dekker, New York, 1979.
11. Looze, D. P., Weiss, J. L., Etemo, J. S., and Barrett, N. M, “An automatic redesign approach for restructurable control systems”, IEEE Control Systems Magazine, 1985, 5(2), 16-22.
12. Morse, W. D., and Ossman, K. A., “Model following reconfigurable flight control system for the AFTI/F-16”, Journal of Guidance, Dynamics and Control, 1990, 13, 969-976.
13. Ostroff, A. J., “Techniques for accommodating control effector Mures on a mildly statically unstable airplane”, Proceedings of the American Control Conference, 1985, 903-906.
14. Napolitano, M R., and Swaim, R. L., “Redesign of the feedback structure following a battle damage and/or a failure on a control surface by eigen structure assignment”, Proceedings of the AIAA Guidance and Control Conference, 1991,247-254.