Adaptive anti-windup control of post-capture combination via tethered space robot

被引:9
作者
Lu, Yingbo [1 ,2 ]
Huang, Panfeng [1 ,2 ]
Meng, Zhongjie [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Res Ctr Intelligent Robot, 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 robot; Dynamic uncertainty; Control input saturation; Adaptive anti-windup; Post-capture combination; NONLINEAR-SYSTEMS; ATTITUDE-CONTROL; TENSION CONTROL; SATELLITE; DEBRIS; DEPLOYMENT; REMOVAL; ROBUST; SWAY;
D O I
10.1016/j.asr.2019.05.029
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Stabilization control is an essential mission for the tethered space robot-target combination during the post-capture phase of tethered space robot (TSR). With the consideration of the space tether and the three dimensional attitude of the post-capture combination, dynamic model of the combination is derived by using Lagrange method. Considering the unknown dynamic parameters (the tether attachment point, unknown target inertia parameters) of the post-capture combination, an adaptive anti-windup control approach is presented to overcome the problem of dynamic uncertainty and control input saturation. Complete stability and performance analyses are presented and illustrative simulation results of application to the post-capture combination system verify the effectiveness of the proposed algorithm. (C) 2019 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:847 / 860
页数:14
相关论文
共 33 条
  • [11] Adaptive control for space debris removal with uncertain kinematics, dynamics and states
    Huang, Panfeng
    Zhang, Fan
    Meng, Zhongjie
    Liu, Zhengxiong
    [J]. ACTA ASTRONAUTICA, 2016, 128 : 416 - 430
  • [12] Adaptive Postcapture Backstepping Control for Tumbling Tethered Space Robot-Target Combination
    Huang, Panfeng
    Wang, Dongke
    Meng, Zhongjie
    Zhang, Fan
    Guo, Jian
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (01) : 150 - 155
  • [13] Fractional order sliding mode control for tethered satellite deployment with disturbances
    Kang, Junjie
    Zhu, Zheng H.
    Wang, Wei
    Li, Aijun
    Wang, Changqing
    [J]. ADVANCES IN SPACE RESEARCH, 2017, 59 (01) : 263 - 273
  • [14] A Hybrid Reliability-Based Design Optimization Approach with Adaptive Chaos Control Using Kriging Model
    Li, Gang
    Meng, Zeng
    Hao, Peng
    Hu, Hao
    [J]. INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2016, 13 (01)
  • [15] Finite time attitude takeover control for combination via tethered space robot
    Lu, Yingbo
    Huang, Panfeng
    Meng, Zhongjie
    Hu, Yongxin
    Zhang, Fan
    Zhang, Yizhai
    [J]. ACTA ASTRONAUTICA, 2017, 136 : 9 - 21
  • [16] Detumbling of Space Debris by a Net and Elastic Tether
    O'Connor, William J.
    Hayden, Deborah J.
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (07) : 1832 - 1839
  • [17] COBRA contactless detumbling
    Peters, Thomas V.
    Olmos, Diego Escorial
    [J]. CEAS SPACE JOURNAL, 2016, 8 (03) : 143 - 165
  • [18] Review and comparison of active space debris capturing and removal methods
    Shan, Minghe
    Guo, Jian
    Gill, Eberhard
    [J]. PROGRESS IN AEROSPACE SCIENCES, 2016, 80 : 18 - 32
  • [19] Optimal Deployment of a Tethered Satellite using Tension Control
    Steindl, Alois
    [J]. IFAC PAPERSONLINE, 2015, 48 (01): : 53 - +
  • [20] Fractional-Order Tension Control Law for Deployment of Space Tether System
    Sun, Guanghui
    Zhu, Z. H.
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2014, 37 (06) : 2062 - 2066