AB - © 2016 Engineers Australia. This paper proposes a fault detection algorithm for the roll dynamic model of a generic delta-wing aircraft. It is assumed that the system model has some noise/uncertainties and the measured roll angle and roll rate used by the control law are faulty/under attack. The proposed fault detection algorithm employs a fault detection estimator and adaptive thresholds to detect the occurrence of a fault in the sensor measurements. Simulation results are presented to show the performance of the proposed algorithm. AU - Deghat, M AU - Lampiri, E AU - Bishop, AN DA - 2017/03/01 DO - 10.1109/AUCC.2016.7868209 EP - 322 JO - 2016 Australian Control Conference, AuCC 2016 PY - 2017/03/01 SP - 317 TI - Sensor fault detection for the roll dynamic model of a generic delta-wing aircraft Y1 - 2017/03/01 Y2 - 2024/03/28 ER -