Fault Detection and Isolation of a Prototype Helicopter Without Angular Velocity Measurements
摘要
In this paper, we present a fault detection and isolation (FDI) scheme for a prototype helicopter against actuator and sensor faults and without any velocity measurements. We develop an FDI unit consisting of two adaptive interval observers to detect the fault and identify the faulty component. Compared to previous works, the proposed FDI unit can accurately detect and locate the fault with a lower computational burden due to the reduced number of observers. Finally, we validate the effectiveness of the proposed scheme using simulations.