Fuzzy Adaptive Nonsingular Terminal Sliding Mode Control of a Miniature Helicopter

被引:1
作者
Moghaddam, Reihaneh Kardehi [1 ]
Baratpoor, Javad [1 ]
机构
[1] Islamic Azad Univ, Dept Elect Engn, Mashhad branch, Mashhad 91735, Iran
来源
JOURNAL OF AEROSPACE INFORMATION SYSTEMS | 2024年 / 21卷 / 02期
关键词
Helicopters; Proportional Integral Derivative Control; Artificial Intelligence; Unmanned Aerial Vehicle; Terminal Sliding Mode; Fuzzy Control System; Adaptive Control Systems; TRACKING CONTROL DESIGN; FLIGHT CONTROL DESIGN;
D O I
10.2514/1.I011156
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a fuzzy adaptive terminal sliding mode control for an unmanned miniature helicopter including uncertainties and external disturbances, and a terminal sliding surface is utilized to provide faster convergence. Due to the fact that the presented controlled system is facing a singularity problem, the controlling structure is developed to a nonsingular one. In the proposed controlling structure, a continuous nonsingular terminal sliding mode control is combined with an adaptive learning algorithm and fuzzy logic system to estimate the uncertainties; and the parameter adaptation law is obtained based on the Lyapunov stability theorem. Analytical results show that the proposed approach enables a faster and more accurate tracking performance as compared to recent controlling methods.
引用
收藏
页码:140 / 151
页数:12
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