Fuzzy PID-Based Design of Quad-Rotor Tracking System

被引：0
|
作者：
Zhou, Wei [1 ,3 ]
Zhang, Changlong [2 ,3 ]
Li, Lizheng
Cheng, Xinmin
机构：
[1] Cent S Univ, Sch Informat Sci & Engn, Changsha, Hunan, Peoples R China
[2] Hunan Univ, Sch Informat Sci & Engn, Changsha 410082, Hunan, Peoples R China
[3] Hunan Keyshare Informat Technol Co LTD, Changsha, Hunan, Peoples R China
来源：
2015 INTERNATIONAL CONFERENCE ON INFORMATION SCIENCE AND INTELLIGENT CONTROL (ISIC 2015) | 2015年
关键词：
Fuzzy Control; GPS Position; Quad-Rotor; Following Mode; Yaw; Pitch;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
To deal with the low precision and poor real-time performance of the existing Quad-Rotor tracking, a new algorithm is proposed which apply fuzzy PID to Rotorcraft tracking control, to achieve timely and accurate yaw and pitch adjustment. Then compare to the classical PID control method and the stages of P control method, the results show that that the fuzzy PID can accurately adjust the nose heading, quickly tracking, and low overshoot. Lastly design a tracking system, and the algorithm is verified by the actual flight data.
引用
收藏
页码：343 / 349
页数：7
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