The Analysis on Posture Control of Micro Quadrotor Based on PID

Abstract

The posture control of micro quadrotor is the key point in flying stability, in this paper, the structure of quadrotor is analyzed, and the kinetic equation has been deduced, a new proportional-integral-derivative controller (PID) control algorithm has been set up based on the velocity matrix, the parameters are simplified and divide to eight classification due to the value of the error. The simulation experiment has made, and experimental results demonstrate the practicability and effectiveness of the new PID algorithm.