Host: The Japan Society of Mechanical Engineers
Name : [in Japanese]
Date : June 05, 2019 - June 08, 2019
A quad tilt-rotor UAV is a UAV which has capability of independent position and attitude flight by adding actuators to change the thrust direction. However, since the number of actuators increases, the control system becomes complicated. It induces difficulty of gain adjustment for stable flight. In this research, focusing on position control, we aim to develop a control system that does not require trial and error gain adjustment for the quad tilt-rotor UAV, and evaluate its validity with numerical simulation and flight experiment.
