Analysis and design the controller for quadrotors based on PID control method

This paper mainly studies the problem of analysis and design of the PID controller for a quadrotor helicopter with six degrees of freedom. The position control, the attitude control of the PID controller parameters are adjusted, in order to make the final output value of the six degrees of freedom versus the expected value equality. In this way, the control purpose is achieved. Finally, it will go through simulations to test the validity of the conclusion.