摘要
介绍一种发动机传感器故障的检测、隔离及适应方法,并给出某型涡轴发动机的数字仿真实例,说明该方法的有效性和实用性。
A method of failure detection,isolation and accomodation for engine sensors is presented.The method is based on engine component level nonlinear model and extended Kalman filter to obtain optimal estimation values of failed sensors and calculation references of the engine model.This makes engine model adapt to the actual engine perfectly and provides analytical redundancy for the failed sensors.In this case,the reliability of the engine control system is enhanced greatly.A numerical digital simulation of a given turboshaft engine has been accomplished.The results prove the effectiveness and practicability of the present method.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
1997年第2期209-211,共3页
Journal of Aerospace Power
关键词
航空发动机
传感器
故障检测
Aircraft engines Failure detection Sensors