Adaptive Observer-Based Fault Diagnosis with Application to Satellite Attitude Control Systems
ICICIC '07 Proceedings of the Second International Conference on Innovative Computing, Informatio and Control
An Experimental Test Bed for Small Unmanned Helicopters
Journal of Intelligent and Robotic Systems
Observer-based robust fault diagnosis for a class of uncertain nonlinear systems
CCDC'09 Proceedings of the 21st annual international conference on Chinese Control and Decision Conference
Journal of Intelligent and Robotic Systems
A Diagnostic Thau Observer for a Class of Unmanned Vehicles
Journal of Intelligent and Robotic Systems
A Quadrotor Test Bench for Six Degree of Freedom Flight
Journal of Intelligent and Robotic Systems
ICIRA'12 Proceedings of the 5th international conference on Intelligent Robotics and Applications - Volume Part I
Journal of Intelligent and Robotic Systems
Trajectory Control of a Quadrotor Subject to 2D Wind Disturbances
Journal of Intelligent and Robotic Systems
Linear Quadratic Control for Quadrotors UAVs Dynamics and Formation Flight
Journal of Intelligent and Robotic Systems
An Efficient Model Predictive Control Scheme for an Unmanned Quadrotor Helicopter
Journal of Intelligent and Robotic Systems
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A robust Fault Diagnosis (FD) scheme for a real quadrotor Unmanned Aerial Vehicle (UAV) is proposed in this paper. Firstly, a novel Adaptive Thau observer (ATO) is developed to estimate the quadrotor system states and build a set of offset residuals to indicate actuators' faults. Based on these residuals, some rules of Fault Diagnosis (FD) are designed to detect and isolate the faults as well as estimate the fault offset parameters. Secondly, a synthetic robust optimization scheme is presented to improve Fault Estimation (FE) accuracies, three key issues include modeling uncertainties, and magnitude order unbalances as well as noises are addressed. Finally, a typical fault of rotors is simulated and injected into one of four rotors of the quadrotor, and experiments for the FD scheme have been carried out. Unlike former research works on the FD schemes for quadrotors, our proposed FD scheme based on the ATO can not only detect and isolate the failed actuators, but also estimate the fault severities. Regardless of roughness of the real flying data, the FD results still have sufficient FE accuracies.