Title :
Kalman Filtering with Inequality Constraints for Certain Turbofan Engine Sensors Fault Diagnosis
Author :
Qian, Kun ; Pang, Xiangping ; Li, Bangyuan ; Xie, Shousheng
Author_Institution :
First Aeronaut. Inst. of the Air Force, Xinyang
Abstract :
Kalman filters are often used to estimate the state variables of a dynamic system. This paper proposed a method of Kalman filtering with linear inequality constraints and applied to certain turbofan aeroengine sensors fault diagnosis. It not only maintains the state variable estimates within a user-defined limit, but also ensures that the state variable estimates vary smoothly and slowly with time and eliminates noise effectively. At the same time, system unmodeled dynamics and random noise disturbance are taken into account in the turbofan engine model. The linearized filtering results demonstrate Kalman filter can estimate state parameters with an average error of less than 0.3%, and the Kalman filtering with linear inequality constraints performs better than the unconstrained filtering. So the proposed method is highly reliable and highly accurate in fault detection and isolation
Keywords :
Kalman filters; aerospace propulsion; fault diagnosis; jet engines; random noise; sensors; state estimation; Kalman filtering; aerospace propulsion system; fault detection; fault diagnosis; fault isolation; random noise disturbance; system unmodeled dynamics; turbofan engine sensors; Aerodynamics; Engines; Fault diagnosis; Filtering; Force sensors; Kalman filters; Maintenance engineering; Nonlinear filters; Sensor systems; State estimation; Kalman filter; aerospace propulsion system; fault diagnosis; inequality constraints; sensor; turbofan engine;
Conference_Titel :
Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
Conference_Location :
Dalian
Print_ISBN :
1-4244-0332-4
DOI :
10.1109/WCICA.2006.1714109