Anti-tangle control of tethered space robots using linear motion of tether offset

被引:22
作者
Wang, Bingheng [1 ,2 ]
Meng, Zhongjie [1 ,2 ]
Jia, Cheng [1 ,2 ]
Huang, Panfeng [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Res Ctr Intelligent Robot, Sch Astronaut, Xian 710072, Shaanxi, Peoples R China
[2] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Xian 710072, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
Tethered space robots; Underactuated systems; Offset control; Energy-based control; Model predictive control; SLIDING MODE CONTROL; ATTITUDE-CONTROL; UNDERACTUATED SPACECRAFT; ALGORITHM; TUG; STABILIZATION; DYNAMICS; TRACKING; TENSION;
D O I
10.1016/j.ast.2019.03.060
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Removal of uncooperative tumbling targets using tethered space robots is subject to the risk of tether tangling around the targets. A good anti-tangle control should be (1) fuel-saving, (2) implementation-friendly and (3) tether-libration-suppressing. The proposed strategy achieves these requirements by using a linear actuator to move the tether offset. However, the underactuation due to the input constraints and coupling arises as a main technical challenge. We address the issue from the system passivity perspective by constructing the potential energy in terms of the tension torque. This makes the most of the tether characteristic whereby we specify the control objective that steers the target's angular velocity to the tether direction. Then, an energy-based sliding mode motion controller is designed, the parameter of which is optimized using a model predictive controller to satisfy the motion constraint. The tangle-avoidance is further reinforced by adaptively tuning the weight of MPC. A RBF neural network and a extended Kalman filer are also used to render the controller robust to the uncertainties. Simulations with different tumbling rates validate the effectiveness of the method. (C) 2019 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:163 / 174
页数:12
相关论文
共 50 条
[1]  
[Anonymous], 2017, BLOCK BACKSTEPPING D
[2]  
[Anonymous], 2001, NONLINEAR CONTROL UN
[3]   Dynamics of Large Debris Connected to Space Tug by a Tether [J].
Aslanov, Vladimir S. ;
Yudintsev, Vadim V. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2013, 36 (06) :1654-1660
[4]   Rigid-Body Attitude Control USING ROTATION MATRICES FOR CONTINUOUS, SINGULARITY-FREE CONTROL LAWS [J].
Chaturvedi, Nalin A. ;
Sanyal, Amit K. ;
McClamroch, N. Harris .
IEEE CONTROL SYSTEMS MAGAZINE, 2011, 31 (03) :30-51
[5]   Hybrid tension control method for tethered satellite systems during large tumbling space debris removal [J].
Chu, Zhongyi ;
Di, Jingnan ;
Cui, Jing .
ACTA ASTRONAUTICA, 2018, 152 :611-623
[6]   Analysis of the effect of attachment point bias during large space debris removal using a tethered space tug [J].
Chu, Zhongyi ;
Di, Jingnan ;
Cui, Jing .
ACTA ASTRONAUTICA, 2017, 139 :34-41
[7]   Control of Space Debris Using an Elastic Tether and Wave-Based Control [J].
Cleary, Sean ;
O'Connor, William J. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (06) :1392-1406
[8]   SPACECRAFT ATTITUDE-CONTROL AND STABILIZATION - APPLICATIONS OF GEOMETRIC CONTROL-THEORY TO RIGID BODY MODELS [J].
CROUCH, PE .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1984, 29 (04) :321-331
[9]   Passivity-Based Attitude Control on the Special Orthogonal Group of Rigid-Body Rotations [J].
Forbes, James Richard .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2013, 36 (06) :1596-1605
[10]   Energy-Based Control Design of an Underactuated 2-Dimensional TORA System [J].
Gao, Bingtuan ;
Zhang, Xiaohua ;
Chen, Hongjun ;
Zhao, Jianguo .
2009 IEEE-RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, 2009, :1296-1301