Adaptive Finite-Time Control for Spacecraft Hovering Over an Asteroid

被引：33
|
作者：
Lee, Daero [1 ]
Vukovich, George [1 ]
机构：
[1] York Univ, Dept Earth & Space Sci & Engn, Lassonde Sch Engn, 4700 Keele St,150 Atkinson Coll, N York, ON M3J 1P3, Canada
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2016年 / 52卷 / 03期
关键词：
SLIDING-MODE CONTROL; TRACKING CONTROL; ORBITS; STABILITY;
D O I：
10.1109/TAES.2015.140822
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper presents a means of near asteroid hovering of a rigid spacecraft in the asteroid body-fixed frame with parameter variations and external disturbances. An adaptive finite-time control scheme is proposed, where the upper bounds of the parametric uncertainties and disturbances are not required for controller design. The detailed design principles and a rigorous stability analysis are provided. Finally, a body-fixed hovering maneuver is employed in numerical simulation to verify the effectiveness of the proposed strategy.
引用
收藏
页码：1183 / 1196
页数：14
相关论文
共 50 条
  • [1] Finite-Time Control for Spacecraft Body-Fixed Hovering Over an Asteroid
    Lee, Daero
    Sanyal, Amit K.
    Butcher, Eric A.
    Scheeres, Daniel J.
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2015, 51 (01) : 506 - 520
  • [2] Finite-time control of underactuated spacecraft hovering
    Huang, Xu
    Yan, Ye
    Huang, Zherui
    [J]. CONTROL ENGINEERING PRACTICE, 2017, 68 : 46 - 62
  • [3] Finite-Time Control Based On The Time-Varying Sliding Mode For Spacecraft Body-Fixed Hovering Over an Asteroid
    Zhao, Jinsong
    Sheng, Yongzhi
    Zeng, Xiangyuan
    Lei, Zhirong
    [J]. PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 3781 - 3786
  • [4] Finite-time control for asteroid hovering and landing via terminal sliding mode guidance
    Yang, Hongwei
    Bai, Xiaoli
    Baoyin, Hexi
    [J]. ACTA ASTRONAUTICA, 2017, 132 : 78 - 89
  • [5] Adaptive Finite-Time Control for Attitude Tracking of Rigid Spacecraft
    Gao, Jiwei
    Cai, Yuanli
    [J]. JOURNAL OF AEROSPACE ENGINEERING, 2016, 29 (04)
  • [6] Distributed adaptive finite-time configuration control of spacecraft formation
    Sun, Yanchao
    Li, Chuanjiang
    Dong, Dingran
    Liu, Mengmeng
    [J]. PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 8649 - 8655
  • [7] Adaptive Finite-Time Attitude Tracking Control for Spacecraft With Disturbances
    Zhao, Lin
    Yu, Jinpeng
    Yu, Haisheng
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2018, 54 (03) : 1297 - 1305
  • [8] Adaptive Finite-time chaotic control of attitude motion of spacecraft
    Lei Tengfei
    Fu Haiyan
    Zhang Yanping
    [J]. 2019 CHINESE AUTOMATION CONGRESS (CAC2019), 2019, : 3567 - 3570
  • [9] Adaptive finite-time attitude coordination control or spacecraft formation
    Lin, Yang
    Wang, Xin
    Lyu, Jianting
    Zhang, Shangjun
    [J]. 2018 IEEE 8TH ANNUAL INTERNATIONAL CONFERENCE ON CYBER TECHNOLOGY IN AUTOMATION, CONTROL, AND INTELLIGENT SYSTEMS (IEEE-CYBER), 2018, : 781 - 785
  • [10] Adaptive double-saturated control for hovering over an asteroid
    Zhang, Bo
    Cai, Yuanli
    Li, Fei
    [J]. ADVANCES IN SPACE RESEARCH, 2019, 63 (07) : 2035 - 2051
12345