Real-Time Adaptive Intelligent Control System for Quadcopter Unmanned Aerial Vehicles With Payload Uncertainties

被引:58
作者
Muthusamy, Praveen Kumar [1 ]
Garratt, Matthew [1 ]
Pota, Hemanshu [1 ]
Muthusamy, Rajkumar [2 ,3 ]
机构
[1] Univ New South Wales, Sch Engn & Informat Technol, Canberra, ACT 2612, Australia
[2] Khalifa Univ Sci & Technol, Khalifa Univ Ctr Autonomous Robot Syst, Abu Dhabi 127788, U Arab Emirates
[3] Khalifa Univ Sci & Technol, Mech Engn Dept, Abu Dhabi 127788, U Arab Emirates
关键词
Uncertainty; Biological neural networks; Payloads; Control systems; Orbits; Adaptation models; Brain modeling; Brain emotional learning based intelligent controller (BELBIC); flight control system; proportional-integral-derivative (PID); quadrotor; UAV; reinforcement learning; six degrees-of-freedom (6DOF); suspended payload uncertainty; wind disturbance; fuzzy neural network (FNN); QUADROTOR UAV; TRACKING; IMPLEMENTATION; DESIGN; MODEL;
D O I
10.1109/TIE.2021.3055170
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A novel bidirectional fuzzy brain emotional learning (BFBEL) controller is proposed to control a class of uncertain nonlinear systems such as the quadcopter unmanned aerial vehicle (QUAV). The proposed BFBEL controller is nonmodel-based and has a simplified fuzzy neural network structure and adapts with a novel bidirectional brain emotional learning algorithm. It is applied to control all six degrees-of-freedom of a QUAV for accurate trajectory tracking and to handle the payload uncertainties and disturbances in real-time. The trajectory tracking performance and the ability to handle the payload uncertainties are experimentally demonstrated on a QUAV. The experimental results show a superior performance and rapid adaptation capability of the proposed BFBEL controller. The proposed BFBEL controller can be used for the commercial drone applications.
引用
收藏
页码:1641 / 1653
页数:13
相关论文
共 38 条
[1]   Emotional learning:: A computational model of the amygdala [J].
Balkenius, C ;
Morén, J .
CYBERNETICS AND SYSTEMS, 2001, 32 (06) :611-636
[2]   DIGITAL-SIMULATION OF ATMOSPHERIC-TURBULENCE FOR DRYDEN AND VONKARMAN MODELS [J].
BEAL, TR .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1993, 16 (01) :132-138
[3]  
BISHEBAN M, 2019, ARXIV190302091
[4]   Robust Backstepping Sliding-Mode Control and Observer-Based Fault Estimation for a Quadrotor UAV [J].
Chen, Fuyang ;
Jiang, Rongqiang ;
Zhang, Kangkang ;
Jiang, Bin ;
Tao, Gang .
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2016, 63 (08) :5044-5056
[5]   Nonlinear Control of Quadrotor for Point Tracking: Actual Implementation and Experimental Tests [J].
Choi, Young-Cheol ;
Ahn, Hyo-Sung .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2015, 20 (03) :1179-1192
[6]   Swing-attenuation for a quadrotor transporting a cable-suspended payload [J].
Eusebia Guerrero-Sanchez, M. ;
Alberto Mercado-Ravell, D. ;
Lozano, Rogelio ;
Daniel Garcia-Beltran, C. .
ISA TRANSACTIONS, 2017, 68 :433-449
[7]  
Fresk E, 2013, 2013 EUROPEAN CONTROL CONFERENCE (ECC), P3864
[8]  
Garratt M. A., 2007, THESIS
[9]  
Glauert H, 1926, ROY AERONAUTICAL SOC, V1127
[10]   Geometric Control of a Quadrotor UAV Transporting a Payload Connected via Flexible Cable [J].
Goodarzi, Farhad A. ;
Lee, Daewon ;
Lee, Taeyoung .
INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2015, 13 (06) :1486-1498