Backstepping-based Attitude Maneuver Control and Active Vibration Reduction of Flexible Spacecraft

被引：2
|
作者：
Zhu, Liangkuan [1 ]
Liu, Yaqiu [1 ]
Wang, Dailin [1 ]
Hu, Qinglei [2 ]
机构：
[1] NE Forestry Univ, Harbin, Heilongjiang Pr, Peoples R China
[2] Harbin Inst Technol, Dept Control Sci & Engn, Harbin, Heilongjiang Pr, Peoples R China
来源：
2008 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-11 | 2008年
关键词：
Flexible spacecraft; Backstepping; Attitude maneuvering;
D O I：
10.1109/CCDC.2008.4597441
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A novel hybrid robust control design method is investigated for a three-axis-rotational maneuver and vibration stabilization of a spacecraft with flexible appendages. Based on the backstepping, a robust attitude control law is derived to control the attitude motion of spacecraft. For actively suppressing the induced vibration, strain rate feedback control methods are presented by using piezoelectric materials as additional sensors and actuators bonded on the surface of the flexible appendages. Numerical simulations demonstrate the feasibility and effectiveness of the control strategy.
引用
收藏
页码：887 / +
页数：2
相关论文
共 50 条
  • [1] A hybrid control scheme of vibration reduction of flexible spacecraft during attitude maneuver
    Shi, Zhong
    Ma, Guangfu
    Hu, Qinglei
    [J]. ISSCAA 2006: 1ST INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1AND 2, 2006, : 169 - +
  • [2] ACTIVE VIBRATION SUPPRESSION IN FLEXIBLE SPACECRAFT DURING ATTITUDE MANEUVER
    Wang, Zhaohui
    Xu, Ming
    Xu, Shijie
    Jia, Shiyuan
    Zhang, Guoqi
    [J]. SPACEFLIGHT MECHANICS 2016, PTS I-IV, 2016, 158 : 733 - 744
  • [3] Backstepping-based adaptive attitude stabilization of a spacecraft
    Li, Chuanjiang
    Ma, Guangfu
    Song, Bin
    [J]. ICIEA 2007: 2ND IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS, VOLS 1-4, PROCEEDINGS, 2007, : 2802 - 2806
  • [4] Variable structure attitude maneuver and vibration control of flexible spacecraft
    胡庆雷
    马广富
    [J]. Journal of Harbin Institute of Technology(New series), 2008, (05) : 705 - 710
  • [5] Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver
    Hu, QL
    Ma, GF
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2005, 9 (04) : 307 - 317
  • [6] Command Filtered Backstepping-Based Attitude Containment Control for Spacecraft Formation
    Zhao, Lin
    Yu, Jinpeng
    Shi, Peng
    [J]. IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2021, 51 (02): : 1278 - 1287
  • [7] Agile attitude maneuver with active vibration-suppression for flexible spacecraft
    Zhang, Jianqiao
    Kong, Xianglong
    Liu, Chuang
    Deng, Qing
    Shi, Keke
    [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2022, 359 (03): : 1172 - 1195
  • [8] Frequency Shaping Backstepping Robust Attitude Maneuver of Flexible Spacecraft
    Liu Shuhao
    Lv Zheng
    [J]. 2018 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS, ROBOTICS AND AUTOMATION (ICMRA), 2018, : 42 - 46
  • [9] Active Vibration Suppression of Flexible Spacecraft During Attitude Maneuver With Actuator Dynamics
    Xu, Shijie
    Cui, Naigang
    Fan, Youhua q
    Guan, Yingzi
    [J]. IEEE ACCESS, 2018, 6 : 35327 - 35337
  • [10] Predictive control for the attitude maneuver of a flexible spacecraft
    Bang, HC
    Oh, CS
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2004, 8 (05) : 443 - 452
12345