Active fault tolerant control based on interval type-2 fuzzy sliding mode controller and non linear adaptive observer for 3-DOF laboratory helicopter

被引:33
|
作者
Zeghlache, Samir [1 ]
Benslimane, Tarak [2 ]
Bouguerra, Abderrahmen [1 ]
机构
[1] Univ Msila, Fac Technol, LASS Lab, Dept Elect, BP 166 Ichbilia, Msila, Algeria
[2] Univ MSila, Fac Technol, Dept Elect Engn, BP 166 Ichbilia, Msila, Algeria
关键词
Type-2 fuzzy logic; Sliding mode controller; Fault tolerant control; 3-DOF helicopter; Non linear observer; Stability; ATTITUDE-CONTROL; SYSTEMS; DESIGN;
D O I
10.1016/j.isatra.2017.09.006
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, a robust controller for a three degree of freedom (3 DOF) helicopter control is proposed in presence of actuator and sensor faults. For this purpose, Interval type-2 fuzzy logic control approach (IT2FLC) and sliding mode control (SMC) technique are used to design a controller, named active fault tolerant interval type-2 Fuzzy Sliding mode controller (AFTIT2FSMC) based on non-linear adaptive observer to estimate and detect the system faults for each subsystem of the 3-DOF helicopter. The proposed control scheme allows avoiding difficult modeling, attenuating the chattering effect of the SMC, reducing the rules number of the fuzzy controller. Exponential stability of the closed loop is guaranteed by using the Lyapunov method. The simulation results show that the AFTIT2FSMC can greatly alleviate the chattering effect, providing good tracking performance, even in presence of actuator and sensor faults. (C) 2017 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:280 / 303
页数:24
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