Actuator Fault Decoupled Residual Generation on Lateral Moving Aircraft

Abstract

Implementation of time-scheduled maintenance is not suitable if it is applied for systems with many varieties of heavy workload and harsh environment since on that condition components degrade earlier that those under normal condition. Therefore it has been shifted to condition-based maintenance (CBM). One important aspect, among others, toward implementation of CBM method is fault isolation. The problem investigated in this paper is related todecouple residual generation for actuator fault isolation of an aircraft on lateral movement. The proposed solution for that problem is to implement combination of transformation matrix and special filter. Transformation matrix is used to convert feature locations of actuator faults to signature vectors. Moreover, the signature vectors will be processed further by special filter to generate decoupled residuals. It is assumed that the actuator is the only fault when the aircraft is on lateral movement. The result showed that special filter and transformation matrix can be designed so that the residual of aileron actuator fault is decoupled from the residual of rudder actuator fault.

Estimasi Deviasi Parameter pada Motor DC Menggunakan Sliding-Mode Observer dan Algoritme Least-Square

“…The model-based maintenance can also be adopted to identify the fault's location inside the plant. For example, the methods for detecting a fault related to the plant's input (actuator fault signal detection) have been proposed in [13]- [16], whereas the methods for detecting a fault related to the plant's output (sensor fault signal detection) have been proposed in [17]- [20]. Other than in actuator (input) and sensor (output), the fault might also occur inside the plant due to the deviation of the plant's parameters from their nominal values.…”