Discrete-Time Sliding Mode Control for Deployment of Tethered Space Robot With Only Length and Angle Measurement

被引:56
作者
Ma, Zhiqiang [1 ,2 ]
Huang, Panfeng [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Sch Astronaut, Xian 710072, Peoples R China
[2] Northwestern Polytech Univ, Res Ctr Intelligent Robot, Sch Astronaut, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
Space vehicles; Aerospace electronics; Extraterrestrial measurements; Robots; Aerodynamics; Stability analysis; Length measurement; Discrete-time sliding mode control (DSMC); discrete-time system; input saturation; tethered space robot (TSR); underactuated system; STABILIZATION; DESIGN;
D O I
10.1109/TAES.2019.2917490
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper proposes a nonlinear discrete-time sliding mode based tension control for deployment of tethered space robot with only length and angle measurements. The discrete-time dynamics of deployment is uncovered based on discretization of Hamilton's principle. Taking into account the underactuated dynamics, the proposed discrete-time sliding surface can generate a specified reduced-order system, which can be regarded as an uncertain discrete-time system with multiple time delays, which is caused by a considerable sample interval, and the stability of a reduced-order system is well analyzed by combining a linear matrix inequation technique based on robust control theory and nonlinear discrete-time Lyapunov method. A novel input structure with the auxiliary variable sequence is presented to deal with the tension saturation, and the states can converge to the specified reduced-order system although the input saturation occurs. The proposed discrete-time method makes no appeal to velocity terms. It is cost-effective to use the proposed method for the information of length and angle are easily measured rather than that of velocity, and it conduces to low requirements for the measurement ability of sensors. Simulation results verify the stability analyses, and are coincident with the stability analyses.
引用
收藏
页码:585 / 596
页数:12
相关论文
共 23 条
[1]  
Bloch AM, 2005, IEEE DECIS CONTR P, P6579
[2]   Post-capture vibration suppression of spacecraft via a bio-inspired isolation system [J].
Dai, Honghua ;
Jing, Xingjian ;
Wang, Yu ;
Yue, Xiaokui ;
Yuan, Jianping .
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2018, 105 :214-240
[3]  
Gao Hui-Jun, 2004, Acta Automatica Sinica, V30, P789
[4]   Advanced tether experiment deployment failure [J].
Gates, SS ;
Koss, SM ;
Zedd, MF .
JOURNAL OF SPACECRAFT AND ROCKETS, 2001, 38 (01) :60-68
[5]   Dexterous Tethered Space Robot: Design, Measurement, Control, and Experiment [J].
Huang, Panfeng ;
Zhang, Fan ;
Cai, Jia ;
Wang, Dongke ;
Meng, Zhongjie ;
Guo, Jian .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2017, 53 (03) :1452-1468
[6]   Experiments and numerical simulations of an electrodynamic tether deployment from a spool-type reel using thrusters [J].
Iki, Kentaro ;
Kawamoto, Satomi ;
Morino, Yoshiki .
ACTA ASTRONAUTICA, 2014, 94 (01) :318-327
[7]  
Kang J., 2018, P AM CONTR C, P646
[8]   Tether tension control law design during orbital transfer via small-gain theorem [J].
Liu, Helong ;
He, Yingzi ;
Yan, Han ;
Tan, Shuping .
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 63 :191-202
[9]   Pure-tension non-linear sliding mode control for deployment of tethered satellite system [J].
Ma, Zhiqiang ;
Sun, Guanghui ;
Cheng, Zhihao ;
Li, Zhengkai .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (13) :2541-2551
[10]   Dynamic adaptive saturated sliding mode control for deployment of tethered satellite system [J].
Ma, Zhiqiang ;
Sun, Guanghui ;
Li, Zhengkai .
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 66 :355-365