Active fault-tolerant control scheme of aerial manipulators with actuator faults

被引:11
作者
Ding, Ya-dong [1 ]
Wang, Yao-yao [1 ,2 ]
Jiang, Su-rong [1 ]
Chen, Bai [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Natl Key Lab Sci & Technol Helicopter Transmiss, Nanjing 210016, Peoples R China
[2] Zhejiang Univ, State Key Lab Fluid Power & Mechatron Syst, Hangzhou 310027, Peoples R China
基金
中国国家自然科学基金;
关键词
aerial manipulators; back-stepping technology; fault-tolerant control; non-singular terminal sliding mode control; extended state observer; SLIDING MODE CONTROL; SYSTEM-DESIGN;
D O I
10.1007/s11771-021-4644-7
中图分类号
TF [冶金工业];
学科分类号
0806 ;
摘要
In this paper, an active fault-tolerant control (FTC) strategy of aerial manipulators based on non-singular terminal sliding mode (NTSM) and extended state observer (ESO) is proposed. Firstly, back-stepping technology is adopted as the control framework to ensure the global asymptotic stability of the closed-loop system. Next, the NTSM with estimated parameters of actuator faults is used as main robustness controller to deal with actuator faults. Then, the ESO is utilized to estimate and compensate the complex coupling effects and external disturbances. The Lyapunov stability theory can guarantee the asymptotic stability of aerial manipulators system with actuator faults and external disturbances. The proposed FTC scheme considers both actuator fault and modelling errors, combined with the adaptive law of actuator fault, which has better performance than traditional FTC scheme, such as NTSM. Finally, several comparative simulations are conducted to illustrate the effectiveness of the proposed FTC scheme.
引用
收藏
页码:771 / 783
页数:13
相关论文
共 30 条
[1]   Experimental Test of a Two-Stage Kalman Filter for Actuator Fault Detection and Diagnosis of an Unmanned Quadrotor Helicopter [J].
Amoozgar, M. Hadi ;
Chamseddine, Abbas ;
Zhang, Youmin .
JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2013, 70 (1-4) :107-117
[2]   Reconfiguration of flight control systems for actuator failures [J].
Bajpai, G ;
Chang, BC ;
Lau, A .
IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 2001, 16 (09) :29-33
[3]   Quadrotor vehicle control via sliding mode controller driven by sliding mode disturbance observer [J].
Besnard, Lenaick ;
Shtessel, Yuri B. ;
Landrum, Brian .
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2012, 349 (02) :658-684
[4]   Robust fixed-time attitude stabilization control of flexible spacecraft with actuator uncertainty [J].
Cao, Lu ;
Xiao, Bing ;
Golestani, Mehdi .
NONLINEAR DYNAMICS, 2020, 100 (03) :2505-2519
[5]   Nonlinear Friction and Dynamical Identification for a Robot Manipulator with Improved Cuckoo Search Algorithm [J].
Ding, Li ;
Li, Xingcheng ;
Li, Qilin ;
Chao, Yuan .
JOURNAL OF ROBOTICS, 2018, 2018
[6]   A practical time-delay control scheme for aerial manipulators [J].
Ding, Yadong ;
Wang, Yaoyao ;
Chen, Bai .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2021, 235 (03) :371-388
[7]   A New 6-DOF Quadrotor Manipulation System: Design, Kinematics, Dynamics, and Control [J].
Fanni, Mohamed ;
Khalifa, Ahmed .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2017, 22 (03) :1315-1326
[8]   STABILITY OF THE PSEUDO-INVERSE METHOD FOR RECONFIGURABLE CONTROL-SYSTEMS [J].
GAO, ZQ ;
ANTSAKLIS, PJ .
INTERNATIONAL JOURNAL OF CONTROL, 1991, 53 (03) :717-729
[9]   A Novel Robotic Platform for Aerial Manipulation Using Quadrotors as Rotating Thrust Generators [J].
Hai-Nguyen Nguyen ;
Park, Sangyul ;
Park, Junyoung ;
Lee, Dongjun .
IEEE TRANSACTIONS ON ROBOTICS, 2018, 34 (02) :353-369
[10]   Sliding mode control applied to reconfigurable flight control design [J].
Hess, RA ;
Wells, SR .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2003, 26 (03) :452-462