Vibration suppression for flexible satellite during attitude stabilization

被引：0
|
作者：
Benmansour, Jalal Eddine [1 ]
Khouane, Boulanouar [2 ]
Roubache, Rima [1 ]
机构：
[1] Ctr Dev Satellites, Dept Rech Mecan Spatiale, Oran, Algeria
[2] Ctr Dev Satellites, Dept Mission & Syst Spatiaux, Oran, Algeria
来源：
PROCEEDINGS 2018 3RD INTERNATIONAL CONFERENCE ON ELECTRICAL SCIENCES AND TECHNOLOGIES IN MAGHREB (CISTEM) | 2018年
关键词：
vibration suppression; Flexible spacecraft; Attitude stabilization; Proportional Derivative; SPACECRAFT; TRACKING;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
This paper treats the problem of vibration mode and attitude control stabilization of a spacecraft with flexible appendage based on state feedback controller (SFC) and vibration suppression using disturbance observer (DO). The spacecraft has a central rigid body and large flexible appendage. The unwanted coupling torques in attitude dynamics that is generated by the vibration of large flexible appendage can affect the performance of attitude stabilization systems. By intergrading DO with SFC, the vibration torques can be reduced and the performance of the desired dynamic can be guaranteed. The Simulation results for flexible spacecraft are given to demonstrate the excellent performance of the composite control approach.
引用
收藏
页码：352 / 355
页数：4
相关论文
共 50 条
  • [1] Collaborative attitude stabilization and distributed vibration suppression of satellite with ultra–large flexible antenna
    Wang, Beichao
    Zhang, Ziyang
    Deng, Xingting
    Li, Shuang
    Xin, Ming
    [J]. Aerospace Science and Technology, 2024, 155
  • [2] Vibration suppression of flexible spacecraft during attitude control
    Song, GB
    Agrawal, BN
    [J]. ACTA ASTRONAUTICA, 2001, 49 (02) : 73 - 83
  • [3] Vibration suppression of flexible spacecraft during attitude maneuvers
    Hu, QL
    Ma, GF
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2005, 28 (02) : 377 - 380
  • [4] Attitude fault tolerant control and active vibration suppression of flexible satellite during orbit control
    Yang, Jing
    Hou, Jian-Wen
    Shi, Xiao-Ping
    [J]. Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2015, 49 (09): : 1373 - 1379
  • [5] Inertia-free attitude stabilization for flexible spacecraft with active vibration suppression
    Liu, Chuang
    Yue, Xiaokui
    Shi, Keke
    Sun, Zhaowei
    [J]. INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2019, 29 (18) : 6311 - 6336
  • [6] 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
  • [7] Active Control Design Approach for Roll/Yaw Attitude Satellite Stabilization with Flexible Vibration
    B. J. Eddine
    Kh. Boulanouar
    [J]. Automatic Control and Computer Sciences, 2020, 54 : 70 - 79
  • [8] Active Control Design Approach for Roll/Yaw Attitude Satellite Stabilization with Flexible Vibration
    Eddine, B. J.
    Boulanouar, Kh.
    [J]. AUTOMATIC CONTROL AND COMPUTER SCIENCES, 2020, 54 (01) : 70 - 79
  • [9] Neural Adaptive Fixed-Time Attitude Stabilization and Vibration Suppression of Flexible Spacecraft
    Yao, Qijia
    Jahanshahi, Hadi
    Moroz, Irene
    Alotaibi, Naif D.
    Bekiros, Stelios
    [J]. MATHEMATICS, 2022, 10 (10)
  • [10] Sampled-data H∞ control for attitude stabilization and vibration suppression of flexible spacecrafts
    Zhu, Baolong
    Zhang, Zhiping
    Suo, Mingliang
    Yu, Zhenhua
    Li, Shunli
    [J]. PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 6376 - 6381
12345