Robust Cerebellar Model Articulation Controller Design for Flight Control Systems
This paper presents a robust proportionalderivative
(PD) based cerebellar model articulation
controller (CMAC) for vertical take-off and landing flight
control systems. Successful on-line training and recalling
process of CMAC accompanying the PD controller is
developed. The advantage of the proposed method is mainly
the robust tracking performance against aerodynamic
parametric variation and external wind gust. The
effectiveness of the proposed algorithm is validated through
the application of a vertical takeoff and landing aircraft
control system.
[1] S. N. Singh, A. A. R. Coelho, "Nonlinear control of mismatched
uncertain linear systems and application to control of aircraft," ASME
Journal of Dynamic Systems, Measurement, and Control, vol. 106, pp.
203-210, 1984.
[2] W. E. Schmitendorf, "Design methodology for robust stabilizing
controllers," Journal of Guidance, vol. 10, pp. 250-254, 1987.
[3] J. Hauser, S. Sastry, and G. Meyer,"Nonlinear control design for slightly
non-minimum phase systems: application to V/STOL aircraft,"
Automatica, vol. 28, no. 4, pp. 665-679, 1992.
[4] F. Lin, W. Zhang, and R. D. Brandt, "Robust hovering control of a
PVTOL aircraft," IEEE Trans. Control System Technology, vol. 7, no. 3,
pp. 343-351, 1999.
[5] M. Saeki and Y. Sakaue, "Flight control design for nonlinear
non-minimum phase VTOL aircraft via two-step linearization," in Proc.
40th IEEE Conf. Decision and Control, 2001, pp. 217-222.
[6] Raymond W. Prouty, Helicopter performance, stability, and control,
Krieger, 2002.
[7] K. D. Do, Z. P. Jiang, and J. Pan, "On global tracking control of a VTOL
aircraft without velocity measurements," IEEE Trans. Automatic Control,
vol. 48, no. 12, pp. 2212-2217, 2003.
[8] Y. J. Huang, T. C. Kuo, H. K. Way, "Robust vertical takeoff and landing
aircraft control via integral sliding mode," IEE Proceedings - Control
Theory and Applications, vol. 150, no. 4, pp. 383-388, 2003.
[9] K. H. Ang, G. Chong, and Y. Lin, "PID control system analysis, design,
and technology," IEEE Trans. Control System Technology, vol. 13, no. 4,
pp. 559-576, 2005.
[10] B. Polajzer, J. Ritonja, G. "tumberger, D. Dolinar, and J. P. Lecointe,
"Decentralized PI/PD position control for active magnetic bearings,"
Electrical Engineering, vol. 89, no. 1, pp. 53-59, 2006.
[11] H. Shiraishi, S. L. Ipri, D. D.Cho, "CMAC neural network controller for
fuel-injection systems," IEEE Trans. Control System Technology, vol. 3,
no. 1, pp. 32-38, 1995.
[12] R. J. Wai, C. M. Lin, and Y. F. Peng, "Robust CMAC neural network
control for LLCC resonant driving linear piezoelectric ceramic motor,"
IEE Proceedings - Control Theory and Applications, vol. 150, no. 3, pp.
221-232, 2003.
[13] C. H. Tsai, "CMAC-based speed estimation method for sensorless vector
control of induction motor drive," Electrical Power Components Systems,
vol. 34, no. 11, pp. 1213-1230, 2006.
[14] C. S. Lin and C. T. Chiang, "Learning convergence of CMAC
technology," IEEE Trans. Neural Network, vol. 8, no. 6, pp. 1281-1292,
1997.
[1] S. N. Singh, A. A. R. Coelho, "Nonlinear control of mismatched
uncertain linear systems and application to control of aircraft," ASME
Journal of Dynamic Systems, Measurement, and Control, vol. 106, pp.
203-210, 1984.
[2] W. E. Schmitendorf, "Design methodology for robust stabilizing
controllers," Journal of Guidance, vol. 10, pp. 250-254, 1987.
[3] J. Hauser, S. Sastry, and G. Meyer,"Nonlinear control design for slightly
non-minimum phase systems: application to V/STOL aircraft,"
Automatica, vol. 28, no. 4, pp. 665-679, 1992.
[4] F. Lin, W. Zhang, and R. D. Brandt, "Robust hovering control of a
PVTOL aircraft," IEEE Trans. Control System Technology, vol. 7, no. 3,
pp. 343-351, 1999.
[5] M. Saeki and Y. Sakaue, "Flight control design for nonlinear
non-minimum phase VTOL aircraft via two-step linearization," in Proc.
40th IEEE Conf. Decision and Control, 2001, pp. 217-222.
[6] Raymond W. Prouty, Helicopter performance, stability, and control,
Krieger, 2002.
[7] K. D. Do, Z. P. Jiang, and J. Pan, "On global tracking control of a VTOL
aircraft without velocity measurements," IEEE Trans. Automatic Control,
vol. 48, no. 12, pp. 2212-2217, 2003.
[8] Y. J. Huang, T. C. Kuo, H. K. Way, "Robust vertical takeoff and landing
aircraft control via integral sliding mode," IEE Proceedings - Control
Theory and Applications, vol. 150, no. 4, pp. 383-388, 2003.
[9] K. H. Ang, G. Chong, and Y. Lin, "PID control system analysis, design,
and technology," IEEE Trans. Control System Technology, vol. 13, no. 4,
pp. 559-576, 2005.
[10] B. Polajzer, J. Ritonja, G. "tumberger, D. Dolinar, and J. P. Lecointe,
"Decentralized PI/PD position control for active magnetic bearings,"
Electrical Engineering, vol. 89, no. 1, pp. 53-59, 2006.
[11] H. Shiraishi, S. L. Ipri, D. D.Cho, "CMAC neural network controller for
fuel-injection systems," IEEE Trans. Control System Technology, vol. 3,
no. 1, pp. 32-38, 1995.
[12] R. J. Wai, C. M. Lin, and Y. F. Peng, "Robust CMAC neural network
control for LLCC resonant driving linear piezoelectric ceramic motor,"
IEE Proceedings - Control Theory and Applications, vol. 150, no. 3, pp.
221-232, 2003.
[13] C. H. Tsai, "CMAC-based speed estimation method for sensorless vector
control of induction motor drive," Electrical Power Components Systems,
vol. 34, no. 11, pp. 1213-1230, 2006.
[14] C. S. Lin and C. T. Chiang, "Learning convergence of CMAC
technology," IEEE Trans. Neural Network, vol. 8, no. 6, pp. 1281-1292,
1997.
@article{"International Journal of Mechanical, Industrial and Aerospace Sciences:61275", author = "Y. J. Huang and T. C. Kuo and B. W. Hong and B. C. Wu", title = "Robust Cerebellar Model Articulation Controller Design for Flight Control Systems", abstract = "This paper presents a robust proportionalderivative
(PD) based cerebellar model articulation
controller (CMAC) for vertical take-off and landing flight
control systems. Successful on-line training and recalling
process of CMAC accompanying the PD controller is
developed. The advantage of the proposed method is mainly
the robust tracking performance against aerodynamic
parametric variation and external wind gust. The
effectiveness of the proposed algorithm is validated through
the application of a vertical takeoff and landing aircraft
control system.", keywords = "vertical takeoff and landing, cerebellar modelarticulation controller, proportional-derivative control.", volume = "5", number = "7", pages = "1448-5", }