Abstract:This paper presents an actuator fault reconstruction system for civil aircraft. The fault reconstruction uses the 'local' actuator model and the sensor measurements. Five different actuator benchmark faults are considered: liquid and solid Oscillatory Failure Case (OFC), liquid and solid jamming, and runaway. The OFC reconstruction is regarded as an input fault reconstruction and is achieved by designing an Iterated Optimal Two-Stage Extended Kalman Filter (IOTSEKF) whereas jamming and runaway faults are consi… Show more
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