A novel hybrid back-stepping and fuzzy logic control strategy for a quadcopter

被引:4
|
作者
Shraim, H. [1 ]
Harkouss, Y. [1 ]
Bazzi, H. [1 ]
机构
[1] Lebanese Univ, Fac Engn 3, Beirut, Lebanon
来源
AERONAUTICAL JOURNAL | 2017年 / 121卷 / 1244期
关键词
Quadrotor modelling; Integral Back-stepping; Fuzzy Logic; STABILIZATION;
D O I
10.1017/aer.2017.70
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article aims to present a novel control strategy for quadrotor helicopter. It is composed of three main parts constituting the system modelling, the integral back-stepping control, and fuzzy logic compensator. In the first part, a non-linear model is presented taking in consideration some non-linearities and variables that are usually neglected. In the second part, a controller based on the integral back-stepping algorithm has been developed for the system in order to make the system follows a desired path. However, due to complexity of paths and to the presence of unknown disturbances, a fuzzy logic compensator is added in parallel to the integral back-stepping controller to improve trajectory tracking in some critical conditions (high wind speed, mass variation, etc.). Simulation results have been presented to show the effectiveness of the proposed approach.
引用
收藏
页码:1444 / 1463
页数:20
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