Akyürek, Ş.; Özden, G.S.; Atlas, E.; Kasnakoğlu, Coşku; Kaynak, Ü.
(International Journal Of Mechanical Engineering And Robotics Research, 2016)
In this paper a Hardware-In-the-Loop (HIL) test platform is used to design a flight stabilization system for Unmanned Aerial Vehicles (UAV). Controllers are first designed and tested separately for lateral and longitudinal ...