TY - GEN
T1 - Sensor/Control Surface Fault Diagnosis and Reconfiguration in Aircraft Control Systems
AU - Hajiyev, Ch
AU - Caliskan, F.
PY - 2004
Y1 - 2004
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=1942439122&partnerID=8YFLogxK
U2 - 10.1061/40722(153)25
DO - 10.1061/40722(153)25
M3 - Conference contribution
AN - SCOPUS:1942439122
SN - 0784407223
SN - 9780784407226
T3 - Engineering Construction and Operations in Challenging Environments Earth and Space 2004: Proceedings of the Ninth Biennial ASCE Aerospace Division International Conference
SP - 176
EP - 183
BT - Engineering, Construction and Operations in Challenging Environments - Earth and Space 2004
PB - ASCE - American Society of Civil Engineers
T2 - Engineering, Construction and Operations in Challenging Environments - Earth and Space 2004: Proceedings of the Ninth Biennial ASCE Aerospace Division International Conference
Y2 - 7 March 2004 through 10 March 2004
ER -