Fault-tolerant reconfiguration of flight control system based on pseudo-inverse and optimal method

• Civil Aviation • Previous Articles Next Articles

Fault-tolerant reconfiguration of flight control system based on pseudo-inverse and optimal method

SHI Zhi-bo^1a,2,SUN Dan^1b.LIU Tao^1a

(1a. Robotics Institute,Aeronautical Automation College;1b. Civil Aircraft Airworthiness and Maintenance Key Lab of Tianjin,CAUC,Tianjin 300300,China;2. Electrical Engineering and Automation College,Harbin Institute of Technology,Harbin 150001,China)

Received:2014-06-03 Revised:2014-07-13 Online:2014-12-25 Published:2014-12-05

Abstract

Abstract:

For the problem of fault-tolerant reconfiguration and handling quality requirements under damaged or failed aircraft control surface,a fault-tolerant reconfiguration project is given for multivariable flight control system based on the linear quadratic optimal regulator (LQR)and pseudo-inverse method. LQR is applied to achieve the stability and optimal design of flight control system,the general description form is established to every fault type,then the control law reconfiguration is realized with pseudo-inverse method and the optimal design is achieved by LQR theory simultaneously. The strictly positive real and global asymptotic stability of the closedloop control system is ensured. Aiming at typical faults,the reconfiguration scheme is verified by computer simulation,which demonstrates that the scheme could ensure effective control of the aircraftwith actuators faults.

Key words: flight control system, pseudo-inverse method, linear quadratic regulator, fault-tolerant reconfiguration, multivariable control

CLC Number:

SHI Zhi-bo,SUN Dan.LIU Tao. Fault-tolerant reconfiguration of flight control system based on pseudo-inverse and optimal method[J]. .

References

[1] 陈宗基，张汝麟，张平，等. 飞行器控制面临的机遇与挑战[J].自动化学报，2013，39（6）：703-710.

[2] 金小峥，杨光红，常晓恒，等. 容错控制系统鲁棒和自适应补偿设计[J].自动化学报，2013，39（1）：31-42.

[3] BUSTAN D，SANI S K H，PARIZ N. Immersion and Invariance Based Fault Tolerant Adaptive Spacecraft Attitude Control[C]//Electrical Engineering（ICEE），2013 21st Iranian Conference on. IEEE，2013：1-6.

[4] HAMAYUN M T，EDWARDS C，ALWIH. A fault tolerant control allocation scheme with output integral sliding modes[J]. Automatica，2013，49（6）：1830-1837.

[5] 张爱华，胡庆雷，霍星，等. 过驱动航天器飞轮故障重构与姿态容错控制[J].宇航学报，2013，34（3）：369-376.

[6] STEPHEN E REIMAN，CHARLES H DILLON，HOWARD P LEE，et al. Adaptive Reconfigurable Dynamic Inversion Control for a Hypersonic Cruise Vehicle[C]//Guidance，Navigation and Control Conference and Exhibit. Honolulu，Hawaii，2008，8（8）：1-11.

[7] 夏小野，王新民，赵凯瑞.伪逆法在飞控系统自修复控制中的应用[J].火力与指挥控制，2010，35（9）：109-112.

[8] 张世杰，赵亚飞，陈闽，等.过驱动轮控卫星的动态控制分配方法[J].航空学报，2011，32（7）：1260-1268.

[9] 唐雅娟，晁福青.伪逆法在自修复飞行控制中的应用研究[J]. 装备指挥技术学院学报，2005，16（4）：73-76.

[10] 范金华，郑志强，吕鸣. 基于伪逆控制分配的过驱动系统稳定性分析[J].信息与控制，2011，40（3）：302-306.

[11] CIUBOTARU B D，STAROSWIECKI M，CHRISTOV N D. Modified Pseudo-Inverse Method with Generalized Linear Quadratic Regulator for fault tolerant Model Matching with prescribed stability degree[C]//Decision and Control and European Control Conference （CDC-ECC），2011 50th IEEE Conference on. IEEE，2011：1583-1588.

[12] 张平，陈宗基. 非线性飞控系统的控制可重构性[J]. 飞机设计，2001（3）：12-15.

[13] STAROSWIECKI M.FaultTolerantControl：thePseudo-Inverse Method Revisited[C]//16th IFAC World Congress，2005.