Reel-Based Tension Control of Tethered Space Robots

被引:9
|
作者
Wang, Bingheng [1 ]
Meng, Zhongjie [2 ,3 ]
Jia, Cheng [2 ,3 ]
Huang, Panfeng [2 ,3 ]
机构
[1] Southern Univ Sci & Technol, Dept Mech & Energy Engn, Inst Robot, Shenzhen 518055, Peoples R China
[2] Northwestern Polytech Univ, Res Ctr Intelligent Robot, Sch Astronaut, Xian 710072, Peoples R China
[3] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
Orbits; Space vehicles; Aerospace electronics; Collision avoidance; Robot sensing systems; Estimation; Active debris removal; model predictive control; system estimation; tension control; tethered space robot; DEBRIS; DESIGN;
D O I
10.1109/TAES.2019.2958156
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article elaborates on the tension control design of tethered space robots for debris removal. The novel approach is to change the tether natural length via a reel. With only the tension sensing, we leverage a Kalman filter and a recursive least-squares algorithm to estimate the actual length and the debris mass, which are fed back to a model-predictive controller to generate the optimal tangential velocity of the reel. Simulations show that the stiff tether exhibits better tension-tracking performance which is robust to the tumbling debris.
引用
收藏
页码:3028 / 3043
页数:16
相关论文
共 50 条
  • [21] Digital deployment control of a tethered satellite system with constrained tension
    Xu, Shidong
    Chen, Ti
    Wen, Hao
    Jin, Dongping
    ADVANCES IN SPACE RESEARCH, 2023, 72 (10) : 4184 - 4196
  • [22] LPV-Based Offline Model Predictive Control for Free-Floating Space Robots
    Jin, Rongyu
    Rocco, Paolo
    Chen, Xueqin
    Geng, Yunhai
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2021, 57 (06) : 3896 - 3904
  • [23] Learning-Based Sliding-Mode Control for Underactuated Deployment of Tethered Space Robot With Limited Input
    Ma, Zhiqiang
    Huang, Panfeng
    Lin, Yuxin
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2022, 58 (03) : 2026 - 2038
  • [24] Discrete-Time Sliding Mode Control for Deployment of Tethered Space Robot With Only Length and Angle Measurement
    Ma, Zhiqiang
    Huang, Panfeng
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2020, 56 (01) : 585 - 596
  • [25] Optimal control scheme of space tethered system for space debris deorbit
    Li, Pengjie
    Zhong, Rui
    Lu, Shan
    ACTA ASTRONAUTICA, 2019, 165 : 355 - 364
  • [26] Finite time attitude takeover control for combination via tethered space robot
    Lu, Yingbo
    Huang, Panfeng
    Meng, Zhongjie
    Hu, Yongxin
    Zhang, Fan
    Zhang, Yizhai
    ACTA ASTRONAUTICA, 2017, 136 : 9 - 21
  • [27] Contact Dynamics and Control for Tethered Space Net Robot
    Zhao, Yakun
    Huang, Panfeng
    Zhang, Fan
    Meng, Zhongjie
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2019, 55 (02) : 918 - 929
  • [28] Simple tension control strategy for variable length tethered satellite system
    School of Astronautics, Beihang University, Beijing 100191, China
    Zhongguo Kongjian Kexue Jishu, 2009, 6 (66-73):
  • [29] Fractional order tension control for stable and fast tethered satellite retrieval
    Sun, Guanghui
    Zhu, Z. H.
    ACTA ASTRONAUTICA, 2014, 104 (01) : 304 - 312
  • [30] Event-Based Predefined-Time Deployment Control for Space Triangular Tethered Satellite System With Input Quantization
    Huang, Bingxiao
    Zhang, Fan
    Song, Mengshi
    Huang, Panfeng
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2023, 59 (05) : 4936 - 4946