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Fault-Tolerant Networked Control Systems Using Control Allocation for Failures in Multiple Control Surfaces

다중 제어면 고장에 대한 제어면 재분배 고장 대처 기법

  • 양인석 (경북대학교 경북대학교 IT대학 국방수중통신/탐지특화연구센터) ;
  • 김동길 (경북대학교 대학원 전자전기컴퓨터학부) ;
  • 이동익 (경북대학교 IT대학)
  • Received : 2011.08.20
  • Accepted : 2011.09.25
  • Published : 2011.11.01

Abstract

In this paper, the methodology of a CA (Control Allocation) based FTNCS (Fault-Tolerant Networked Control System) is proposed. Control allocation is a control surface management technique by redistributing the redundant control surfaces in overactuated systems. In modern high performance aircrafts, they adopt many redundant control surfaces to provide high performance and to satisfy various tactical requirements. Moreover, redundant control surfaces provide an opportunity to compensate performance degradation due to failures in more than one actuator by re-allocating redundant control surfaces. Simulation results with an F-18 HARV demonstrate that the proposed CA based FTNCS can achieve a fast and accurate tracking performance even in the presence of actuator faults.

Keywords

References

  1. Z. Gao and P. J. Antsaklis, "Stability of the pseudo-inverse method for reconfigurable control systems," International Journal of Control, vol. 53, no. 3, pp. 717-729, 1991. https://doi.org/10.1080/00207179108953643
  2. K. J. Åström and B. Wittenmark, Adaptive Control, 2nd Ed.,Addison-Wesley Publishing Company, Inc., 1995.
  3. I. Yang, Y. Kim, and D. Lee, "Actuator failure diagnosis and accommodation using sliding mode control for submersible vehicle," Journal of Institute of Control, Robotics and Systems (in Korean), vol. 16, no. 7, pp. 661-667, 2010. https://doi.org/10.5302/J.ICROS.2010.16.7.661
  4. J. D. Boskovic and R. K. Mehra, "A multiple model-based reconfigurable flight control system design," Proc. the 37th IEEE Conference on Decision & Control, pp. 4503-4508, Dec. 1998.
  5. D. Enns, "Control allocation approaches," AIAA Guidance, Navigation and Control Conference and Exhibit, pp. 98-108, 1998.
  6. J. Buffington, P. Chandler, and M. Pachter, "On-line system identification for aircraft with distributed control effectors," International Journal of Robust and Nonlinear Control, vol. 9, no. 14, pp. 1033-1049, 1999. https://doi.org/10.1002/(SICI)1099-1239(19991215)9:14<1033::AID-RNC451>3.0.CO;2-#
  7. H. Alwi and C. Edwards, "Fault tolerant control using sliding modes with on-line control allocation," Automatica, vol. 44, pp. 1859-1866, 2008. https://doi.org/10.1016/j.automatica.2007.10.034
  8. K. Ahmed and T. Didier, "Reconfigurable control design for over-actuated systems based on reliability indicators," Conference on Control and Fault Tolerant Systems, Nice, France, Oct. 2010.
  9. I. Yang, D. Kim, and D. Lee, "Fault-tolerant control strategy based on control allocation using smart actuators," Conference on Control and Fault Tolerant Systems, Nice, France, pp. 377- 381, Oct. 2010.
  10. K. W. Iliff and K. -S. C. Wang, "Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring," NASA/TP-97-206539, 1997.
  11. Y. Zhang and J. Jiang, "Bibliographical review on reconfigurable fault-tolerant control systems," Proc. of the 5th IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes 2003, Washington, D. C., USA, pp. 265-276, 2003.
  12. D. Lee, "Distributed real-time fault-tolerant control using smart actuators and time-triggered communication," Ph.D. Dissertation, Dept. Automatic Control & Systems Eng., Sheffield University, UK, 2002.
  13. C. Kambhampati, R. J. Patton, and F. J. Uppal, "Reconfiguration in networked control systems: fault tolerant control and plugand- play," 6th IFAC Symposium on Fault Detection, Supervision and Safety of Technical Processes, Tsinghua University, P. R. China, pp. 151-156, 2006.
  14. J. D. Boskovic and R. K. Mehra, "Failure detection, identification and reconfiguration in flight control," Fault Diagnosis and Fault Tolerance for Mechatronic Systems: Recent Advances, Springer-Verlag, 2002.
  15. J. A. Richard, J. M. Buffington, A. G. Sparks, and S. S. Banda, Robust Multivariable Flight Control, London: Springer-Verlag, 1994.
  16. D. Enns, D. Bugajski, R. Hendrick, and G. Stein, "Dynamic inversion: an evolving methodology for flight control design," Int. J. Cont., vol. 59, no. 1, pp. 71-91, 1994. https://doi.org/10.1080/00207179408923070
  17. "Military Standard Flying Qualities of Piloted Aircraft," Mil- STD-1797A, Jan. 1990.

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