TWQH Attitude Control Experiments on Horizon Ground Simulator and Flight Test

Abstract

This paper presents the results of two experiments on the Horizon ground simulator and outdoor flight test of TWQH hybrid UAV in presence of wind perturbation. The simulation results show the stability and error boundedness of the PID controller while the experimental inflight tests indicate the good performances of the proposed controller.

Keywords

• hybrid uav
• hover
• attitude control
• flight test
• stability
• pid regulator