Neural Observer-Based Intelligent Fault-Tolerant Control of Multi-Helicopters Under Actuator Faults: A Fully Actuated System Approach

被引:0
作者
Miao, Qiyang [1 ]
Xia, Jingping [1 ]
Jiang, Bin [1 ,2 ]
Zhang, Ke [1 ,2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Peoples R China
[2] Natl Key Lab Helicopter Aeromech, Nanjing, Peoples R China
来源
2024 3RD CONFERENCE ON FULLY ACTUATED SYSTEM THEORY AND APPLICATIONS, FASTA 2024 | 2024年
基金
中国国家自然科学基金;
关键词
Helicopters; actuator faults; formation control; fault-tolerant control; fully actuated system approach; SPACECRAFT;
D O I
10.1109/FASTA61401.2024.10595330
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 investigates the fault-tolerant formation control of multiple unmanned helicopters under actuator faults through a neural-based fully actuated system approach (FASA). First, the kinematic and dynamic model of the helicopter with actuator faults is established, from which the fully actuated system description of a helicopter is derived. Second, to mitigate the dependence on model accuracy, a neural observer is designed to approximate the lumped uncertainty including the nonlinear, coupling, and faulty terms of a helicopter. Third, based on the estimated system dynamic, a triple-layered FASA controller is proposed to achieve the leader-follower formation control of helicopters. Finally, numerical simulations are conducted to validate the efficiency of the proposed algorithm.
引用
收藏
页码:565 / 570
页数:6
相关论文
共 16 条
[1]   Adaptive Fuzzy Fault-Tolerant Control of High-Order Nonlinear Systems: A Fully Actuated System Approach [J].
Cui, Yang ;
Duan, Guangren ;
Liu, Xiaoping ;
Zheng, Hongyu .
INTERNATIONAL JOURNAL OF FUZZY SYSTEMS, 2023, 25 (05) :1895-1906
[2]   Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach [J].
Duan Guangquan ;
Liu Guo-Ping .
JOURNAL OF SYSTEMS SCIENCE & COMPLEXITY, 2022, 35 (02) :623-640
[3]   Integrated Fault Estimation and Accommodation Design for Discrete-Time Takagi-Sugeno Fuzzy Systems With Actuator Faults [J].
Jiang, Bin ;
Zhang, Ke ;
Shi, Peng .
IEEE TRANSACTIONS ON FUZZY SYSTEMS, 2011, 19 (02) :291-304
[4]   Hybrid three-dimensional formation control for unmanned helicopters [J].
Karimoddini, Ali ;
Lin, Hai ;
Chen, Ben M. ;
Lee, Tong Heng .
AUTOMATICA, 2013, 49 (02) :424-433
[5]   Intelligent Leader-Following Consensus Formation Control Using Recurrent Neural Networks for Small-Size Unmanned Helicopters [J].
Kuo, Chia-Wei ;
Tsai, Ching-Chih ;
Lee, Chi-Tai .
IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2021, 51 (02) :1288-1301
[6]   Integrated fault-tolerant control for a 3-DOF helicopter with actuator faults and saturation [J].
Lan, Jianglin ;
Patton, Ron J. ;
Zhu, Xiaoyuan .
IET CONTROL THEORY AND APPLICATIONS, 2017, 11 (14) :2232-2241
[7]  
Liu G., 2023, Guidance, Navigation and Control
[8]   Neuroadaptive Cooperative Fault-Tolerant Control of Heterogeneous Multiagent Systems Based on Fully Actuated System Approaches [J].
Ma, Yonghao ;
Zhang, Ke ;
Jiang, Bin .
IEEE TRANSACTIONS ON CYBERNETICS, 2024, 54 (08) :4581-4592
[9]   Aggressive control of helicopters in presence of parametric and dynamical uncertainties [J].
Marconi, Lorenzo ;
Naldi, Roberto .
MECHATRONICS, 2008, 18 (07) :381-389
[10]   Non-Iterative nonlinear model predictive approach applied to the control of helicopters' group formation [J].
Saffarian, M. ;
Fahimi, F. .
ROBOTICS AND AUTONOMOUS SYSTEMS, 2009, 57 (6-7) :749-757