Journal of Institute of Control, Robotics and Systems (제어로봇시스템학회논문지)

Institute of Control, Robotics and Systems (제어로봇시스템학회)
권호 표지
DOI QR코드

DOI QR Code

Analysis on Flight Test Results of Reconfiguration Flight Control System

재형상 비행제어 시스템의 비행시험 결과 분석

  • Published : 2008.12.01
Download PDF
⟨ Previous Next ⟩

Abstract

This paper presents the analysis results obtained by the flight test of reconfiguration flight control system for an aircraft. The reconfiguration flight control system was designed by using control allocation scheme that automatically distributes the demanded control moments determined by control law to each actual control surface. In this paper, some control allocation algorithms for reconfiguration control of general aircraft with redundant control surfaces are summarized and their performance evaluation results through nonlinear simulation and Hardware-In-the-Loop-Simulation (HILS) test are shown. Also, Unmanned Aerial Vehicle (UAV) system adopted as a platform for the flight test of reconfiguration flight controller and the implementation procedure of reconfiguration flight controller into real-time UAV system were introduced. Finally, flight test results were analyzed.

Keywords

References

  1. C. N. Jones, 'Reconfigurable Flight Control First Year Report,' University of Cambridge, 2002
  2. G. Tao, S. M. Joshi, and X. Ma, 'Adaptive State Feedback and Tracking Control of Systems with Actuator Failures,' IEEE Trans. on Automatic Control, vol. 46, no. 1, pp. 78-95, January 2001 https://doi.org/10.1109/9.898697
  3. G. Tao, S. Chen, and S. M. Joshi, 'An Adaptive Actuator Failure Compensation Controller Using Output Feedback,' IEEE Trans. on Automatic Control, vol. 47, no. 3, pp. 506-511, March 2002 https://doi.org/10.1109/9.989150
  4. K. S. Kim, K. J. Lee, and Y. Kim, 'Reconfigurable Flight Control System Design Using Direct Adaptive Method,' Journal of Guidance, Control, and Dynamics, vol. 26, no. 4, pp. 543-550, July-Aug. 2003 https://doi.org/10.2514/2.5103
  5. 문관영, 김유단, 이한민, '매개변수 추정 및 모델추종 적응제어기법을 이용한 재형상 비행제어시스템 연구,' 한국항공우주학회지, 제34권, 제3호, pp. 67-73, March 2006
  6. 김부민, 김병수, 김응태, 박무혁, '신경회로망을 이용한 재형상 비행제어법칙 설계,' 한국항공우주학회지, 제34권, 제7호, pp. 35-44, July 2006
  7. A. A. Pashilkar, N. Sundararajan, and P. Saratchandran, 'Adaptive Nonlinear Neural Controller for Aircraft Under Actuator Failures,' Journal of Guidance, Control, and Dynamics, vol. 30, no. 3, pp. 835-847, May-June 2007 https://doi.org/10.2514/1.26540
  8. S. Suzuki and A. Yanagida, 'Research and Development for Fault Tolerant Flight Control System - Part 1. Intelligent Flight Control System,' Proc. of the 26th International Congress of the Aeronautical Sciences, Anchorage, Sept. 2008
  9. W. C. Durham, 'Constrained Control Allocation,' Journal of Guidance, Control, and Dynamics, vol. 14, no. 4, pp. 717-725, July-Aug. 1993
  10. W. C. Durham, 'Constrained Control Allocation: Three Moment Problem,' Journal of Guidance, Control, and Dynamics, vol. 17, no. 2, pp. 330-336, March-April 1994 https://doi.org/10.2514/3.21201
  11. J. J. Burken, P. Lu, Z. Wu, and C. Bahm, 'Two Reconfigurable Flight-Control Design Methods: Robust Servomechanism and Control Allocation,' Journal of Guidance, Control, and Dynamics, vol. 24, no. 3, pp. 482-493, May-June 2001 https://doi.org/10.2514/2.4769
  12. W. C. Durham, 'Computational Efficient Control Allocation,' Journal of Guidance, Control, and Dynamics, vol. 24, no. 3, pp. 519-524, May-June 2001 https://doi.org/10.2514/2.4741
  13. M. Bodson, 'Evaluation of Optimization Methods for Control Allocation,' Journal of Guidance, Control, and Dynamics, vol. 25, no. 4, pp. 703-711, July-Aug. 2002 https://doi.org/10.2514/2.4937
  14. O. Harkegard, 'Efficient Active Set Algorithm for Solving Constrained Least Square Problem in Aircraft Control Allocation,' Proc. of the 41th IEEE Conf. on Decision and Control, pp. 1295-1300, 2002
  15. 진재현, 유창선, 류혁, 탁민제, '수정된 의사역행 렬배분배 기법을 이용한 여유 조종력 할당,' 한국항공우주학회지, 제32권, 제9호, pp. 65-71, July 2004
  16. J. Jin, 'Modified Pseudoinverse Redistribution Methods for Redundant Controls Alloatoin,' Journal of Guidance, Control, and Dynamics, vol. 25, no. 5, pp. 1076-1079, Sept.-Oct. 2005
  17. K. Masui, H. Tomita and A. Yanagida, 'Research and Development for Fault Tolerant Flight Control System - Part 2. Flight Experiments,' Proc. of the 26th International Congress of the Aeronautical Sciences, Anchorage, Sept. 2008
  18. V. Gavrilets, 'Damage Tolerant Flight Coltrol Systems for Unmanned Aircraft,' Proc. of the 26th International Congress of the Aeronautical Sciences, Anchorage, Sept. 2008
  19. S. A. Snell, D. F. Enns, and W. L. Garrard Jr., 'Nonlinear Inversion Flight for A Supermaneuverable Aircraft,' Journal of Guidance, Control, and Dynamics, vol. 15, no. 4, pp. 976-984, July-Aug. 1992 https://doi.org/10.2514/3.20932
  20. 민병문, 김응태, 이장호, 탁민제, '두루미-II 무인기 기반의 조종력 할당 기법 성능 평가,' 한국항공우주학회지, 제35권, 제2호, pp. 107-114, Feb. 2007 https://doi.org/10.5139/JKSAS.2007.35.2.107
  21. B. M. Min, B. J. Kim, E. T. Kim and M. J. Tahk, 'Performance Evaluation and HILS Test of Control Allocation Methods for Reconfiguration Control,' Proc. of the 26th International Congress of the Aeronautical Sciences, Anchorage, Sept. 2008