Fault Tolerant Control Based on Direct Adaptive Fuzzy Position Controller for a Helicopter-Like Twin Rotor MIMO System: Design and Real Time Experimentation

被引:0
作者
Zeghlache, Samir [1 ]
Ghellab, Mohammed Zinelaabidine [1 ]
Djerioui, Ali [2 ]
Benyettou, Loutfi [2 ]
Berrabah, Fouad [2 ]
Benkhoris, Mohamed Fouad [3 ]
机构
[1] Univ Msila Univ Pole, Fac Technol, LASS Lab Anal Signaux & Syst, Dept Elect Engn, Rd Bourdj Bou Arreiridj, Msila 28000, Algeria
[2] Univ Msila Univ Pole, Fac Technol, Dept Elect Engn, LGE Lab Genie Elect, Rd Bourdj Bou Arreiridj, Msila 28000, Algeria
[3] Univ Nantes, IREENA Lab, St Nazaire, France
关键词
TRMS; Fuzzy system; Fault tolerant control; Robust control; Adaptive control; Lyapunov stability; SLIDING MODE CONTROL; ATTITUDE-CONTROL; SPACECRAFT;
D O I
10.1007/s40998-025-00793-7
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
In this paper, a direct fuzzy position controller is developed for Twin Rotor MIMO System (TRMS) in robust path following versus actuator faults. This control method relies on estimating an optimal inverse dynamic control to achieve desired trajectory tracking and stability goals. To achieve this objective, a fuzzy system is employed to approximate the ideal inverse dynamic control to the greatest extent feasible. The parameters of the fuzzy system that is employed may be adjusted online according to a stable adaptation rule. The adjustable parameters are created with the aim of reducing the discrepancy between the fuzzy controller and the ideal inverse dynamic control, which is currently unknown. Firstly, the dynamical modelling of the TRMS is carried out. Secondly, a direct fuzzy adaptive control is applied to the TRMS, thirdly, asymptotic stability is proved by utilizing Lyapunov approach. The proposed control is introduced to the TRMS with 2 degree of freedom (DOF) configuration, where the decoupling step is not requiring. Practical results show good trajectory following capability of the developed controller in attendance of actuator faults and parametric variations.
引用
收藏
页码:545 / 569
页数:25
相关论文
共 73 条
  • [11] Robust exponential arbitrary time control of nonlinear systems with input delay
    Derakhshannia, Mehran
    Moosapour, Seyyed Sajjad
    [J]. COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2024, 131
  • [12] Nonlinear Disturbance Observer Based Adaptive Explicit Nonlinear Model Predictive Control Design for a Class of Nonlinear MIMO System
    Dutta, Lakshmi
    Das, Dushmanta Kumar
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2023, 59 (02) : 1965 - 1979
  • [13] Design of an Adaptive Linear Quadratic Regulator for a Twin Rotor Aerodynamic System
    Faisal, Rafal Fawzi
    Abdulwahhab, Omar Waleed
    [J]. JOURNAL OF CONTROL AUTOMATION AND ELECTRICAL SYSTEMS, 2021, 32 (02) : 404 - 415
  • [14] Experimental validation of adaptive RBFNN global fast dynamic terminal sliding mode control for twin rotor MIMO system against wind effects
    Ghellab, Mohammed Zinelaabidine
    Zeghlache, Samir
    Djerioui, Ali
    Benyettou, Loutfi
    [J]. MEASUREMENT, 2021, 168
  • [15] Nonlinear adaptive fault-tolerant control for full-car active suspension with velocity measurement errors and full-state constraints
    Guo, Xuejie
    Wang, Jue
    Sun, Weichao
    [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2024, 361 (10):
  • [16] Adjustable order fault estimation observer based fault-tolerant control for switched fuzzy stochastic systems
    Han, Jian
    Yu, Ping
    Liu, Xiuhua
    Wei, Xinjiang
    [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2024, 361 (16):
  • [17] Switched step integral backstepping control for nonlinear motion systems with application to a laboratory helicopter
    Haruna, A.
    Mohamed, Z.
    Efe, M. O.
    Abdullahi, A. M.
    [J]. ISA TRANSACTIONS, 2023, 141 : 470 - 481
  • [18] Fixed-time fault-tolerant attitude control for flexible spacecraft without angular velocity sensor
    Hasan, Muhammad Noman
    Chen, Yong
    Liang, Jiongjiong
    Wen, An
    [J]. ISA TRANSACTIONS, 2024, 146 : 87 - 98
  • [19] Adaptive sliding mode and RBF neural network based fault tolerant attitude control for spacecraft with unknown uncertainties and disturbances
    Hou, Zhiwei
    Lan, Xuejing
    [J]. ADVANCES IN SPACE RESEARCH, 2024, 74 (04) : 1680 - 1692
  • [20] Adaptive Fuzzy Attitude Sliding Mode Control for a Quadrotor Unmanned Aerial Vehicle
    Huang, Tianpeng
    Gao, Xiaoyang
    Li, Tieshan
    [J]. INTERNATIONAL JOURNAL OF FUZZY SYSTEMS, 2024, 26 (02) : 686 - 701