Adaptive fuzzy fault-tolerant attitude control of spacecraft

Control Engineering Practice

Volumn 19, Issue 1, 2011, Pages 10-21

  Zou, An Min ^a   Kumar, Krishna Dev ^a  

^a RYERSON UNIVERSITY   (Canada)

Author keywords

Actuator failures; Adaptive control; Backstepping; Fuzzy logic; Spacecraft attitude

Indexed keywords

ACTUATOR FAILURES; ADAPTIVE CONTROL; ADAPTIVE FUZZY; ADAPTIVE LAWS; ADAPTIVE MECHANISM; BACKSTEPPING TECHNIQUE; CONTROL INPUT CONSTRAINTS; DIRECT APPROACH; EXTERNAL DISTURBANCES; FAULT-TOLERANT; FUZZY LOGIC SYSTEM; GLOBAL REPRESENTATION; LYAPUNOV; MASS MOMENT; NUMERICAL SIMULATION; PARAMETRIC UNCERTAINTIES; ROBUST ADAPTIVE CONTROLLER; SPACECRAFT ATTITUDE; SYSTEM UNCERTAINTIES; TWO PARAMETER; UNIT QUATERNION; WEIGHT MATRICES;

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; ATTITUDE CONTROL; BACKSTEPPING; CONTROLLERS; FAULT TOLERANT COMPUTER SYSTEMS; FUZZY SYSTEMS; NAVIGATION; SPACECRAFT; SPATIAL VARIABLES CONTROL; UNCERTAINTY ANALYSIS;

FUZZY LOGIC;

EID: 78649924886     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.conengprac.2010.08.005     Document Type: Article

References (24)

1. Akella M.R., Valdivia A. Velocity-free attitude controllers subject to actuator magnitude and rate saturations. Journal of Guidance, Control, and Dynamics 2005, 28(4):659-666.
2. Boskovic J.D., Li S.-M., Mehra R.K. Robust adaptive variable structure control of spacecraft under control input saturation. Journal of Guidance, Control, and Dynamics 2001, 24(1):14-22.
3. Boskovic J.D., Li S.-M., Mehra R.K. Robust tracking control design for spacecraft under control input saturation. Journal of Guidance, Control, and Dynamics 2004, 27(4):627-633.
4. Cai W., Liao X.H., Song Y.D. Indirect robust adaptive fault-tolerant control for attitude tracking of spacecraft. Journal of Guidance, Control, and Dynamics 2008, 31(5):1456-1463.
5. Chan P.T., Rad A.B., Wang J. Indirect adaptive fuzzy sliding mode control, part II: Parameter projection and supervisory control. Fuzzy Sets and System 2001, 122(1):31-43.
6. Chen B.-S., Wu C.-S., Jan Y.-W. Adaptive fuzzy mixed H2/H∞ attitude control of spacecraft. IEEE Transactions on Aerospace and Electronic Systems 2000, 36(4):1343-1359.
7. Choi, M.-T., & Flashner, H. (2000). Neural-network-based spacecraft attitude control. In AIAA guidance, navigation, and control conference and exhibit, Denver, CO.
8. Hornik K., Stinchcombe M., White H. Multilayer feedforward networks are universal approximators. Neural Networks 1989, 2:359-366.
9. Huges P.C. Spacecraft attitude dynamics 1986, Wiley, New York.
10. Kanellakopoulos I., Kokotovic P.V., Morse A.S. Systematic design of adaptive controllers for feedback linearizable systems. IEEE Transactions on Automatic Control 1991, 36(11):1241-1253.
11. Kwan C., Xu H., Lewis F. Robust spacecraft attitude control using fuzzy logic. International Journal of Systems Science 2000, 31(10):1217-1225.
12. Narendra K.S., Annaswamy A.M. A new adaptive law for robust adaptation without persistent excitation. IEEE Transactions on Automatic Control 1987, AC-32(2):134-145.
13. Park Y., Tahk M.-J., Bang H. Design and analysis of optimal controller for fuzzy systems with input constraint. IEEE Transactions on Fuzzy Systems 2004, 12(6):766-779.
14. Qu Z. Robust control of nonlinear uncertain systems 1998, Wiley, New York.
15. Sanner, R. M. (1996). Adaptive attitude control using fixed and dynamically structured neural networks. In AIAA guidance, navigation and control conference, San Diego, CA.
16. Sanner R.M., Slotine J.-J.E. Gaussian networks for direct adaptive control. IEEE Transactions on Neural Networks 1992, 3(6):837-863.
17. Talebi, H. A., & Patel, R. V. (2006). An intelligent fault detection and recovery scheme for reaction wheel actuator of satellite attitude control systems. In Proceedings of IEEE international conference on control applications (pp. 3282-3287), Munich, Germany.
18. Talebi, H. A., Patel, R. V., & Khorasani, K. (2007). Fault detection and isolation for uncertain nonlinear systems with applications to a satellite reaction wheel actuator. In Proceedings of IEEE international conference on systems, man and cybernetics (pp. 3140-3145), Montreal, Quebec, Canada.
19. Tsiotras, P., & Schleicher, A. (2000). Detumbling and partial attitude stabilization of a rigid spacecraft under actuator failure. In AIAA guidance, navigation, and control conference and exhibit, Denver, CO.
20. Wang, L. X. (1992). Fuzzy systems are universal approximators. In Proceedings of IEEE international conference on fuzzy systems (pp. 1163-1170), San Diego, CA, USA.
21. Wang L.X., Mendel J.M. Fuzzy basis function, universal approximation, and orthogonal least-squares learning. IEEE Transactions on Neural Networks 1992, 3(5):807-814.
22. Wu, Q., & Saif, M. (2005). Robust fault diagnosis for satellite attitude systems using neural state space models. In IEEE international conference on systems, man and cybernetics (Vol. 2, pp. 1955-1960).
23. Zhang, K., Jiang, B., & Shi, P. (2007). Adaptive observer-based fault diagnosis with application to satellite attitude control systems. In Proceedings of the second international conference on innovative computing, information and control.
24. Zou A.-M., Kumar K.D., Hou Z.-G. Quaternion-based adaptive output feedback attitude control of spacecraft using Chebyshev neural networks. IEEE Transactions on Neural Networks 2010, 21(9):1457-1471.