• Cover Page
• Editorial Board and Information for Authors
• Aims and Scope
• Contents
Contents
Rotondo D., Nejjari F. and Puig V.
Robust quasi-LPV model reference FTC of a quadrotor UAV subject to
actuator faults . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
Hardier G., Seren C. and Ezerzere P.
Model-based techniques for virtual sensing of longitudinal flight parameters. . . 23
Franzè G., Furfaro A., Mattei M. and Scordamaglia V.
A safe supervisory flight control scheme in the
presence of constraints and anomalies. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .39
Ossmann D. and Varga A.
Detection and identification of loss of efficiency faults of flight actuators . . . . . . . . . . . . . . 53
Rodriguez-Alfaro L., Alcorta-Garcia E., Lara D. and Romero G.
A Hamiltonian approach to fault isolation
in a planar vertical take-off and landing aircraftmodel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65
Glizer V.Y. and Turetsky V.
Increasing pursuer capturability by using hybrid dynamics . . . . . . . . . . . . . . . . . . . . . . . 77
HamayunM.T., Edwards C., Alwi H. and Bajodah A.
A fault tolerant direct control allocation scheme with
integral sliding modes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .93
Hu B. and Seiler P.
A probabilistic method for certification of analytically redundant systems. . . . . . . . . . . . . . . . . . .103
Péni T., Vanek B., Szabó Z. and Bokor J.
Supervisory fault tolerant control of the GTM UAV using LPV
methods . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 117
Yang X. and Maciejowski J.M.
Fault tolerant control using Gaussian processes and model predictive control . . . . . 133
Ariola M., Mattei M., Notaro I., Corraro F. and Sollazzo A.
An SFDI observer-based scheme for a general
aviation aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 149
Cen Z., Noura H. and Younes Y.A.
Systematic fault tolerant control based on adaptive Thau observer estimation
for quadrotorUAVs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .159
Wu C., Qi J., Song D., Qi X. and Han J.
Simultaneous state and parameter estimation based actuator fault
detection and diagnosis for an unmanned helicopter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 175
Ducard G.J.J.
SMAC-FDI: A single model active fault detection and isolation system for unmanned aircraft . . . . . . . 189