Article | 07-April-2018
This paper studies on the dynamics model and control method of quad-rotor UAV for research. Firstly analyzes the dynamic characteristic of quad-rotor UAV and establishes the nonlinear dynamics model of quad-rotor UAV; and then applies the PID control to three channels of pitch, roll and yaw based on the established model, and the simulation results show that PID control is effective for the quad-rotor UAV control with the ideal conditions. Finally analyzes the results of PID control under the
Yang Sen,
Wang Zhongsheng
International Journal of Advanced Network, Monitoring and Controls, Volume 2 , ISSUE 1, 83–89