Title :
The Analysis on Posture Control of Micro Quadrotor Based on PID
Author :
Fang, Shu ; Xu, Yan ; Jiang, Jingxue ; Hu, Bin ; Que, Xinggui
Author_Institution :
Shanghai Fire Inst. of Minist. of Public Security, Shanghai, China
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.
Keywords :
helicopters; position control; stability; three-term control; flying stability; kinetic equation; micro quadrotor; posture control; proportional-integral-derivative controller; velocity matrix; Acceleration; Aircraft; Equations; Kinetic theory; Mathematical model; Robots; Tuning; PID; kinetic equation; micro quadrotor; velocity matrix;
Conference_Titel :
Computational Intelligence and Design (ISCID), 2011 Fourth International Symposium on
Conference_Location :
Hangzhou
Print_ISBN :
978-1-4577-1085-8
DOI :
10.1109/ISCID.2011.173
