| Citation: | CHEN Yi, HUANG Jin-quan, ZHANG Peng. FDIA simulation of aero-engine control system sensor FDIA system[J]. Journal of Aerospace Power, 2008, 23(2): 396-400. |
| [1] |
Delaat J C,Merrill W C.Advanced detection isolation and accommodation of sensor failures in turbofan engine,realtime microcomputer implementation[R].NASA-2925,1990.
|
| [2] |
方昌德.发动机状态监视和故障诊断系统的发展[J].国际航空,2005,6:66-68.FANG Changde.Condition monitoring and fault diagnostic system of engine[J].International Aviation,2005,6:66-68.
|
| [3] |
Sanjay G.Controls and health management technologies for intelligent aerospace propulsion systems[R].AIAA-2004-0949.
|
| [4] |
Takahisa K.Aircraft engine sensor/actuator/componentfault diagnosis using a bank of kalman filters[R].NASA/CR-2003-212298.
|
| [5] |
Takahisa K,Donald L s.Application of a bank of kalman filters for aircraft engine fault diagnostics[R].NASA/TM-2003-212526.
|
| [6] |
李松林,孙健国,李健民,等.涡扇发动机机载自适应建模技术研究[J].航空动力学报,1997,13(3):315-318.LI Songlin,SUN Jianguo,LI Jianmin,et al.An in-flight adaptive model of turbofan[J].Journal of Aerospace Power,1997,13(3):315-318.
|