Sensor/Control Surface Fault Diagnosis and Reconfiguration in Aircraft Control Systems
Sensor/Control Surface Fault Diagnosis and Reconfiguration in Aircraft Control Systems
- Neue Suche nach: Hajiyev, Ch.
- Neue Suche nach: Caliskan, F.
- Neue Suche nach: Hajiyev, Ch.
- Neue Suche nach: Caliskan, F.
In this paper, an approach to detect and isolate the aircraft sensor/control surface faults affecting the mean of the Kalman filter innovation sequence is proposed, and a new structure for a fault tolerant aircraft control system is presented. In the simulations, the longitudinal and lateral dynamics of an F-16 aircraft model is considered, and detection and isolation of pitch rate gyro faults and control surface faults are examined. The principal block diagram of a fault tolerant aircraft control system is illustrated.
Dokumentinformationen
Sensor/Control Surface Fault Diagnosis and Reconfiguration in Aircraft Control Systems
Ninth Biennial Conference on Engineering, Construction, and Operations in Challenging Environments ; 2004 ; League City, Houston, Texas, United States
2004-03-03
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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