Quad-rotor UAV Control Method Based on PID Control Law

被引：11
|
作者：
Yang Sen [1 ,2 ]
Wang Zhongsheng [3 ]
机构：
[1] Ordance Engn Coll, Dept UAV Engn, Shijiazhuang, Hebei, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing, Peoples R China
[3] Xian Technol Univ, Sch Engn & Comp Sci, Xian 710021, Shaanxi, Peoples R China
来源：
2017 INTERNATIONAL CONFERENCE ON COMPUTER NETWORK, ELECTRONIC AND AUTOMATION (ICCNEA) | 2017年
关键词：
quad-rotor; dynamics model; PID;
D O I：
10.1109/ICCNEA.2017.24
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
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 circumstance that the data form feedback channel is polluted by noise, which lay the foundation for the improvement of the PID control law.
引用
收藏
页码：418 / 421
页数：4
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