Reconfigurable tracking control with saturation

Journal of Guidance, Control, and Dynamics

Volumn 18, Issue 5, 1995, Pages 1016-1022

  Pachter, M ^a   Chandler, P R ^b   Mears, M ^b  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT; ALGORITHMS; COMPUTER SIMULATION; CONSTRAINT THEORY; IDENTIFICATION (CONTROL SYSTEMS); LINEAR PROGRAMMING; MATHEMATICAL MODELS; ONLINE SYSTEMS; OPTIMIZATION; PREDICTIVE CONTROL SYSTEMS; TRACKING (POSITION);

AIRCRAFT TRACKING; CONTROL SURFACE FAILURE; HORIZON/MODEL PREDICTIVE OPTIMAL CONTROL; ON-LINE OPTIMIZATION; ON-LINE SYSTEM IDENTIFICATION; RATE SATURATION; RECONFIGURABLE TRACKING CONTROL;

OPTIMAL CONTROL SYSTEMS;

EID: 0029368441     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.21499     Document Type: Article

References (8)

1. Michalska, H., and D. Q. Mayne, “Robust Receding Horizon Control of Constrained Nonlinear Systems,” IEEE Transactions on Automatic Control, Vol. 28, No. 11,1993, pp. 1623-1633.
2. Chandler, P., Pachter, M., and Mears, M., “System Identification for Adaptive and Reconfigurable Control,” Journal of Guidance, Control, and Dynamics, Vol. 18, No. 3, 1993, pp. 516-524.
3. Chandler, P., Mears, M., and Pachter, M., “A Hybrid On-Line Optimization approach for Addressing Actuator Rate Saturation in Reconfigurable Flight Control,” IEEE Transactions on Control System Technology (submitted for publication).
4. Kirk, D. E., Optimal Control Theory, Prentice-Hall, Englewood Cliffs, NJ, 1970.
5. Rao, S. S., Optimization Theory and Applications, Halsted Press, New York, 1984.
6. Rao, S. S., IMSL MATH/LIBRARY Users Manual, Version 2.0, International Mathematical and Statistical Library, Houston, TX, 1991.
7. Chandler, P., Mears, M., and Pachter, M., “A Hybrid LQR/LP Approach for Addressing Actuator Saturation in Feedback Control,” Proceedings of the IEEE Conference on Decision and Control (Orlando, FL), 1994, pp.3860-3867.
8. Hoak, D. E., “USAF Stability and Control DATCOM,” Air Force Wright Aeronautical Lab., AFWAL-TR-83-3048, Wright-Patterson AFB, OH, Oct. 1960 (revised 1978).