Volume 29 Issue 5
May  2003
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Li Weiqi, Chen Zongji. Control Law Reconfiguration under Control Surface Failure  for Nonlinear Aircraft Dynamic[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(5): 428-433. (in Chinese)
Citation: Li Weiqi, Chen Zongji. Control Law Reconfiguration under Control Surface Failure  for Nonlinear Aircraft Dynamic[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(5): 428-433. (in Chinese)

Control Law Reconfiguration under Control Surface Failure  for Nonlinear Aircraft Dynamic

  • Received Date: 01 Mar 2002
  • Publish Date: 31 May 2003
  • The application of pseudo-inverse method based flight control reconfiguration i n the 6 degrees of freedom aircraft model was introduced. The failure considered here is the control surface effectiveness loss or lock-in-place. Via the appro priate linearization of the control coefficients, the reconfiguration problem wa s simplified to a problem of solving a linear equations. The real-time digital simulation results were given to indicate the validity of the algorithm.

     

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  • [1] 张 平,陈宗基.基于伪逆法的自修复飞控系统的控制律重构 . 见:秦化淑. 中国控制 会议文集 . 北京:中国科学技术出版社, 1995. 1746~1754 Zhang Ping, Chen Zongji. Pseudo-inverse method based control reconfiguration in self-repairing flight control system . In:Qin Huashu. Proceeding of the 1 9 95 Chinese Control Conference . Beijing:China Science & Technology Press, 1 995.1746~1754(in Chinese) [2] 邵华章,杨振宇,陈宗基. 伪逆法在飞行控制律重构中的应用[J]. 控制 与决策,1999,14(3):281~284 Shao Huazhang, Yang Zhenyu, Chen Zongji. Application of pseudo-inverse method t o flight control reconfiguration[J]. Control and Decision, 1999, 14(3):281~28 4(in Chinese) [3] 邵华章,陈宗基. 自修复飞控系统设计研究[J]. 北京航空航天大学学报 ,1999,25(1):30~33 Shao Huazhang, Chen Zongji. Self-repairing flight control system design researc h[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25( 1):30~33(in Chinese) [4] 张 平,陈宗基. 飞机操纵面故障研究及其补偿重构[J]. 飞行力学,199 7,15(3):67~72 Zhang Ping, Chen Zongji. Aircraft failures studies and its reconfigurable contro l[J]. Flight Dynamics, 1997, 15(3):67~72(in Chinese) [5] 张 平, 陈宗基. 飞机滚转运动的控制余度与重构效能[J]. 飞行力学, 1 998, 16(3):62~67 Zhang Ping, Chen Zongji. The control redundancy and reconfiguration benefit for an aircraft's roll motion[J]. Flight Dynamics, 1998, 16(3):62~67(in Chinese ) [6] Boskovic J D, Mehra R K. A multiple model-based reconfigurable flight control system design . Proceeding of the 1998 Conference on Decision and Control . Tampa, Florida USA, 1998. 4503~4508 [7] Huzmezan M, Maciejowski J M. Reconfigurable flight control of a high inci dence research model using predictive control .UKACC International Confere ce on CONTROL'98 . Swansea, UK, 1998. 1169~1174 [8] Kim D, Kim Y. Robust variable structure controller design for fault toler ant flight control[J]. AIAA Journal of Guidance, Control, and Dynamics, 2000, 23(3):430~437 [9] Calise J, Lee S, Sharma M. Development of a reconfigurable flight control law for the X-36 tailless fighter aircraft . AIAA Proc Guidance, Navigati on and Control Conference .2000
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