Multi-Fault Diagnosis Approach Based on Updated Interacting Multiple Model for Aviation Hydraulic Actuator
The aviation hydraulic actuator (HA) is a key component of the flight control system in an aircraft. It is necessary to consider the occurrence of multiple faults under harsh conditions during a flight. This study designs a multi-fault diagnosis method based on the updated interacting multiple model...
Main Authors: | Xiaozhe Sun, Xingjian Wang, Siru Lin |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2020-08-01
|
Series: | Information |
Subjects: | |
Online Access: | https://www.mdpi.com/2078-2489/11/9/410 |
Similar Items
-
Fault monitoring in hydraulic systems using unscented Kalman filter
by: Sepasi, Mohammad
Published: (2007) -
Fault monitoring in hydraulic systems using unscented Kalman filter
by: Sepasi, Mohammad
Published: (2007) -
Fault monitoring in hydraulic systems using unscented Kalman filter
by: Sepasi, Mohammad
Published: (2007) -
Simultaneous State and Parameter Estimation Based Actuator Fault Detection and Diagnosis for an Unmanned Helicopter
by: Wu Chong, et al.
Published: (2015-03-01) -
SENSORS FAULT DIAGNOSIS ALGORITHM DESIGN OF A HYDRAULIC SYSTEM
by: Matej ORAVEC, et al.
Published: (2017-06-01)