An integrated FDI and FTC design for an aircraft model

An integrated FDI and FTC design for an aircraft model. Seminar of two hours for the for the Nanjing University of Aeronautics and Astronautics - NUAA
 
 

Abstract

• The talk illustrates the development of an active fault-tolerant control strategy obtained from the integration of a fault detection and diagnosis module with a controller reconfiguration method. The methodology is based on a fault detection and diagnosis procedure relying on adaptive filters designed via a nonlinear approach. The controller reconfiguration mechanism exploited in the control loop depends on the online estimate of the fault signal. The active fault tolerant control scheme is therefore applied to a simulator of an aerial vehicle in several flight conditions, in the presence of actuator faults, turbulence, measurement noise, and modelling errors.

Keywords

• Fault detection and diagnosis, fault detection and isolation, active control, fault-tolerant system, nonlinear geometric approach, aircraft simulator.

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