The design of UAV control system based on DSP

被引：2

作者：

Luo Yun-lin ^{[1
]}

Chen Bao-jie ^{[1
]}

机构：

[1] Civil Aviat Univ China, Aeronaut Automat Coll, Tianjin, Peoples R China

来源：

2012 INTERNATIONAL CONFERENCE ON CONTROL ENGINEERING AND COMMUNICATION TECHNOLOGY (ICCECT 2012) | 2012年

关键词：

unmanned aerial vehicle (UAV); flight control; the fuzzy PID control;

D O I：

10.1109/ICCECT.2012.101

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

According to the unmanned aerial vehicle (UAV) autonomous flight control problem, this paper designs the UAV control system. This paper introduces the system structure and basic functions detailed, and according to the characteristics of the UAV flight control, it designs improvably the fuzzy PID controller, and the results of simulation show that the control method improves the dynamic characteristic and steady precision of UAV. Finally, the system design is reasonable after the flight test, and it can meet the demand of UAV flight control.

引用

页码：527 / 530

页数：4