Fuzzy-PID hybrid control system to navigate an autonomous mini-Quadrotor

被引：0

作者：

Zareb, M. ^{[1
]}

Ayad, R. ^{[1
]}

Nouibat, W. ^{[1
]}

机构：

[1] Univ Sci & Technol, Dept Elect, USTO, Oran, Algeria

来源：

2013 3D INTERNATIONAL CONFERENCE ON SYSTEMS AND CONTROL (ICSC) | 2013年

关键词：

component; Mamdani-type fuzzy controller; PID classic controller Fuzzy control; UAV; Quadrotor; Non-linear systems;

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：

This paper report on the synthesis of a flight control system for an autonomous mini-Quadrotor. This system is developed on the base of realistic non-linear mathematical model. It's consisting of hybrid controllers, two controllers are Mamdani-type fuzzy controllers for attitude control. These fuzzy controllers are designed using a simple rule base. Four conventional SISO PID controllers are also used for roll, pitch, yaw angles and altitude control, Performance issues of flight control system are illustrated in a simulator of the Quadrotor in Matlab Simulink. The results show that the overall system becomes stable and robust.

引用

页数：8

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