20th Annual International Conference on Mechatronics and Machine Vision in Practice, M2VIP 2013, Ankara, Türkiye, 20 Eylül 2013, ss.63-69
In this work, design and flight test prototype of a quadrotor helicopter UAV with sub-rotor control surfaces for non-inclined horizontal motion are described. Initial flight test results acquired from the prototype of the proposed UAV are presented in order to reveal the functionality of the new approach.