... , … , b p ] , where b j ∈ R N × 1 , j = 1 , p ¯ , and the system with actuator faults can be written as: (4) x ( j + 1 ) = A x ( j ) + B f u ( j ) + G w ( j ) Fault detection Fault isolation Kalman filters Filter tuning Innovation...

...-based controller to be used to realize fault isolation completely. Originality/value The fuzzy logic approach applied to the flight control system adds an important key for sensor fault isolation because it reduces the effect of false alarms and allows the identification of different kinds of sensor...

...Huayi Li; Qingxian Jia; Rui Ma; Xueqin Chen Purpose The purpose of this paper is to accomplish robust actuator fault isolation and identification for microsatellite attitude control systems (ACSs) subject to a series of space disturbance torques and gyro drifts. Design/methodology/approach...

... a Kalman filter to obtain without noise, a full order observer for sensor fault detection, a GOS (generalized observer scheme) for sensor fault isolation and a fuzzy controller to reconfigure of the healthy sensor. This combination is simulated using the state space model of a lateral flight control system...