Robust adaptive PID tracking control design for uncertain spacecraft systems: A fuzzy approach

IEEE Transactions on Aerospace and Electronic Systems

Volumn 42, Issue 4, 2006, Pages 1506-1514

  Huang, Guo Shing ^a   Uang, Huey Jian ^b  

^a NATIONAL CHIN YI UNIVERSITY OF TECHNOLOGY   (Taiwan)

^b MINGHSIN UNIVERSITY OF SCIENCE AND TECHNOLOGY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; ATTITUDE CONTROL; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; EIGENVALUES AND EIGENFUNCTIONS; FUZZY LOGIC; SYSTEMS ANALYSIS; THREE TERM CONTROL SYSTEMS; UNCERTAIN SYSTEMS;

FUZZY LOGIC SYSTEM; ROBUST ADAPTIVE CONTROLLER; SPACECRAFT ATTITUDE MANEUVERS; TRACKING CONTROL DESIGN;

SPACECRAFT;

EID: 33947692706     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2006.314591     Document Type: Article

References (16)

1. Dwyer, T. A. W., III. Exact nonlinear control of large angle rotational maneuvers. IEEE Transactions on Automatic Control, AC-29, 9 (1984), 769-774.
2. Singh, S. N., and Bossart, T. C. Feedback linearization and nonlinear ultimate boundedness control of the space station using CMG. In AIAA Guidance, Navigation, and Control Conference, vol. 1, 90-3354-CP, Washington, D.C., 1990, 369-376.
3. Singh, S. N., and Iyer, A. Nonlinear decoupling sliding mode control and attitude control of spacecraft. IEEE Transactions on Aerospace and Electronic Systems, 25, 5 (1989), 621-633.
4. Kim, K. S., and Kim, Y. Robust backstepping control for slew maneuver using nonlinear tracking function. IEEE Transactions on Control System Technology, 11, 6 (2003), 822-829.
5. Junkins, J. L., and Turner, J. D. Optimal continuous torque attitude maneuvers. Journal of Guidance and Control, 3, 3 (1980), 210-217.
6. Byun, K. W., Wie, B., Geller, D., and Sunkel, J. Robust H∞ control design for the space station with structured parameter uncertainty. Journal of Guidance and Control, and Dynamics, 14, 6 (1991), 1115-1122.
7. 2/H∞ approach. Journal of Guidance and Control, and Dynamics, 24, 4 (2001), 755-766.
8. 2/H∞ attitude control of spacecraft. IEEE Transactions on Aerospace and Electronic Systems, 36, 4 (2000), 1343-1359.
9. Kaplan, M. H. Modern Spacecraft Dynamics and Control. New York: Wiley, 1976.
10. Wang, L. X. Adaptive Fuzzy Systems and Control: Design and Stability Analysis. Englewood Cliffs, NJ: Prentice-Hall, 1994.
11. Dorf, R. C., and Bishop, R. H. Modern Control Systems (8th ed.). Reading, MA: Addison-Wesley, 1998.
12. Isidori, A., and Asolfi, A. Disturbance attenuation and H∞ control via measurement feedback in nonlinear systems. IEEE Transactions on Automatic Control, 37 (1992), 1283-1293.
13. Hhalil, H. K. Adaptive output feedback control of nonlinear systems represented by input-output models. IEEE Transactions on Automatic Control, 41, 2 (1996), 177-188.
14. Boyd, S., El Ghaoui, L., Feron, E., and Balakrishnan, V. Linear Matrix Inequalities in System and Control Theory. Philadelphia, PA: SIAM, 1994.
15. Khalil, H. K. Nonlinear Systems. Upper Saddle River, NJ: Prentice-Hall, 1996.
16. Show, L. L., Juang, J. C., Lin, C. T., and Jan, Y. W. Spacecraft robust attitude tracking design: PID control approach. In Proceedings of the American Control Conference, Anchorage, AK, 2002, 1360-1365.