典型文献
Civil aircraft fault tolerant attitude tracking based on extended state observers and nonlinear dynamic inversion
文献摘要：
For the problem of sensor faults and actuator faults in aircraft attitude control,this paper proposes a fault tolerant con-trol(FTC)scheme based on extended state observer(ESO)and nonlinear dynamic inversion(NDI).First,two ESOs are designed to estimate sensor faults and actuator faults respectively.Second,the angular rate signal is reconstructed according to the estimation of sensor faults.Third,in angular rate loop,NDI is de-signed based on reconstruction of angular rate signals and es-timation of actuator faults.The FTC scheme proposed in this pa-per is testified through numerical simulations.The results show that it is feasible and has good fault tolerant ability.
文献关键词：
中图分类号：
作者姓名：
MA Xinjian;LIU Shiqian;CHENG Huihui
作者机构：
School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai 200240,China
文献出处：
引用格式：
[1]MA Xinjian;LIU Shiqian;CHENG Huihui-.Civil aircraft fault tolerant attitude tracking based on extended state observers and nonlinear dynamic inversion)[J].系统工程与电子技术（英文版）,2022(01):180-187
A类：
ESOs
B类：
Civil,aircraft,tolerant,attitude,tracking,extended,state,observers,nonlinear,dynamic,inversion,For,problem,sensor,faults,actuator,control,this,paper,proposes,FTC,scheme,NDI,First,two,are,designed,estimate,respectively,Second,angular,rate,reconstructed,according,estimation,Third,loop,reconstruction,signals,proposed,testified,through,numerical,simulations,results,show,that,feasible,has,good,ability
AB值：
0.447094
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