Fuzzy Sliding Mode Controller Based Trajectory Tracking Control of Free Flying Space Robot Manipulator System

被引:1
作者
Shibabw, Esubalew W. [1 ]
Tamiru, Gerbaw Y. [1 ]
机构
[1] Bahirdar Univ, Bahirdar Inst Technol, Bahir Dar, Ethiopia
来源
ARTIFICIAL INTELLIGENCE AND DIGITALIZATION FOR SUSTAINABLE DEVELOPMENT, ICAST 2022 | 2023年 / 455卷
关键词
FFSRMS; FSMC; OOS; Robust; Trajectory tracking; ADAPTIVE-CONTROL; DYNAMICS;
D O I
10.1007/978-3-031-28725-1_9
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
A free flying space robot manipulator system (FFSRMS) is made up of a six degrees of freedom (DOF) spacecraft and n degree of freedom manipulator mounted on the base spacecraft. The space robot manipulator is used to perform a variety of tasks in space or on orbit service (OOS), such as assembling and repairing spacecraft, refueling satellites in orbit, and removing space debris. Unlike ground-based robot manipulators, a space robot manipulator has no fixed base. As a result, the base and manipulator are strongly coupled. Furthermore, the system operates in unstructured and zero gravity environment. The kinematics and dynamics of a FFSRMS has been developed based on chaseles theorem and Euler-Lagrangian equation of motion respectively. The stability of the system and the convergence of the tracking errors to the origin has been checked using Lyapunov stability criterion. This work used a fuzzy sliding mode controller (FSMC) to examine a space robot manipulator trajectory tracking control capability in joint space and robustness. The proposed controller has been simulated in MATLAB/Simulink considering external disturbance and parametric variation and compared with the sliding mode controller to evaluate how effective it is. The results reveal that the proposed controller is robust and has good trajectory tracking capability with a reduced Integral Time Absolute Error (ITAE) and it eliminate the chattering effect. The comparative study shows that FSMC has reduced ITAE than SMC.
引用
收藏
页码:137 / 158
页数:22
相关论文
共 30 条
[1]   Adaptive Control for a Torque Controlled Free-Floating Space Robot with Kinematic and Dynamic Model Uncertainty [J].
Abiko, Satoko ;
Hirzinger, Gerd .
2009 IEEE-RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, 2009, :2359-2364
[2]  
[Anonymous], About us
[3]   A review of structures, verification, and calibration technologies of space robotic systems for on-orbit servicing [J].
Ding XiLun ;
Wang YeCong ;
Wang YaoBing ;
Xu Kun .
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2021, 64 (03) :462-480
[4]  
Edwards C., 1998, Sliding Mode Control: Theory and Applications
[5]   A review of space robotics technologies for on-orbit servicing [J].
Flores-Abad, Angel ;
Ma, Ou ;
Pham, Khanh ;
Ulrich, Steve .
PROGRESS IN AEROSPACE SCIENCES, 2014, 68 :1-26
[6]   A NORMAL-FORM AUGMENTATION APPROACH TO ADAPTIVE-CONTROL OF SPACE ROBOT SYSTEMS [J].
GU, YL ;
XU, YS .
DYNAMICS AND CONTROL, 1995, 5 (03) :275-294
[7]  
Holkar K. S., 2013, Int. J. Comput. Appl., V78, P1
[8]  
Hughes P.C., 2004, Spacecraft Attitude Dynamics
[9]   Continuous integral sliding mode control for space manipulator with actuator uncertainties [J].
Jia, Shiyuan ;
Shan, Jinjun .
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 106
[10]   On-orbit service (OOS) of spacecraft: A review of engineering developments [J].
Li, Wei-Jie ;
Cheng, Da-Yi ;
Liu, Xi-Gang ;
Wang, Yao-Bing ;
Shi, Wen-Hua ;
Tang, Zi-Xin ;
Gao, Feng ;
Zeng, Fu-Ming ;
Chai, Hong-You ;
Luo, Wen-Bo ;
Cong, Qiang ;
Gao, Zhen-Liang .
PROGRESS IN AEROSPACE SCIENCES, 2019, 108 :32-120