Sensor and Actuator Fault Detection and Isolation for a High Performance Aircraft Engine Bleed Air Temperature Control System
In this brief, an unscented Kalman filter (UKF)-based method is developed to detect and isolate both temperature sensor and valve actuator faults of a high performance aircraft bleed air temperature control system . The proposed method involves two unscented Kalman filters: one is used to detect sen...
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| Veröffentlicht in: | IEEE transactions on control systems technology 2011-09, Vol.19 (5), p.1260-1268 |
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| container_end_page | 1268 |
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| container_title | IEEE transactions on control systems technology |
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| creator | Shang, Lan Liu, Guangjun |
| description | In this brief, an unscented Kalman filter (UKF)-based method is developed to detect and isolate both temperature sensor and valve actuator faults of a high performance aircraft bleed air temperature control system . The proposed method involves two unscented Kalman filters: one is used to detect sensor fault and the other is dedicated to actuator fault detection. Nonlinear state space equations describing the engine bleed air temperature control system test rig dynamics are derived and utilized in the design and convergence analysis of the proposed fault detection and isolation method. Computer simulations and experiments have been conducted, and the proposed fault detection method is shown to be effective in detecting and isolating sensor and actuator faults. |
| doi_str_mv | 10.1109/TCST.2010.2076353 |
| format | Article |
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The proposed method involves two unscented Kalman filters: one is used to detect sensor fault and the other is dedicated to actuator fault detection. Nonlinear state space equations describing the engine bleed air temperature control system test rig dynamics are derived and utilized in the design and convergence analysis of the proposed fault detection and isolation method. Computer simulations and experiments have been conducted, and the proposed fault detection method is shown to be effective in detecting and isolating sensor and actuator faults.</description><identifier>ISSN: 1063-6536</identifier><identifier>EISSN: 1558-0865</identifier><identifier>DOI: 10.1109/TCST.2010.2076353</identifier><identifier>CODEN: IETTE2</identifier><language>eng</language><publisher>New York, NY: IEEE</publisher><subject>Actuators ; Aircraft ; Aircraft propulsion ; Applied sciences ; bleed air ; Bleeding ; Computer science; control theory; systems ; Continuous cycle engines: steam and gas turbines, jet engines ; Control theory. Systems ; Dynamical systems ; Engines and turbines ; Exact sciences and technology ; Fault detection ; fault isolation ; Faults ; Industrial metrology. Testing ; Kalman filtering ; Kalman filters ; Mathematical model ; Mechanical engineering. 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Systems</topic><topic>Dynamical systems</topic><topic>Engines and turbines</topic><topic>Exact sciences and technology</topic><topic>Fault detection</topic><topic>fault isolation</topic><topic>Faults</topic><topic>Industrial metrology. Testing</topic><topic>Kalman filtering</topic><topic>Kalman filters</topic><topic>Mathematical model</topic><topic>Mechanical engineering. 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| ispartof | IEEE transactions on control systems technology, 2011-09, Vol.19 (5), p.1260-1268 |
| issn | 1063-6536 1558-0865 |
| language | eng |
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| source | IEEE Electronic Library (IEL) |
| subjects | Actuators Aircraft Aircraft propulsion Applied sciences bleed air Bleeding Computer science control theory systems Continuous cycle engines: steam and gas turbines, jet engines Control theory. Systems Dynamical systems Engines and turbines Exact sciences and technology Fault detection fault isolation Faults Industrial metrology. Testing Kalman filtering Kalman filters Mathematical model Mechanical engineering. Machine design Modelling and identification Nonlinear dynamics Sensors Temperature control Temperature sensors Valves |
| title | Sensor and Actuator Fault Detection and Isolation for a High Performance Aircraft Engine Bleed Air Temperature Control System |
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