Fault tolerant heading control system design for Turac unmanned aerial vehicle
TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, pp. 267.0-276.0, 2017.
In this study, a fault tolerant heading control system is designed for a one-third scale fixed wing vertical takeoff-and-landing unmanned aerial vehicle, Turac. A nonlinear six degrees-of-freedom (DoF) mathematical model is obtained and linearized at the calculated trim flight condition. A proportional heading control system is designed a...More
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