Design and Simulation of satellite attitude control system based on Simulink

被引:0
|
作者
Zhang, Yang [1 ]
Gan, Qingbo [1 ]
Kang, Jingshu [2 ]
机构
[1] Chinese Acad Sci, Space Syst Dept, Acad Optoelect, Beijing 100094, Peoples R China
[2] China Astronaut Publishing House, Beijing 100048, Peoples R China
关键词
satellite attitude control; visual simulation; earth-oriented; virtual reality;
D O I
10.1117/12.2230844
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
In order to research satellite attitude control system design and visual simulation, the simulation framework of satellite dynamics and attitude control using Simulink were established. The design of satellite earth-oriented control system based on quaternion feedback was completed. The 3D scene based on VR was created and models in the scene were driven by simulation data of Simulink. By coordinate transformation. successful observing the scene in inertial coordinate system, orbit coordinate system and body coordinate system. The result shows that application of simulation method of Simulink combined with VR in the design of satellite attitude control system field, has the advantages of high confidence level, hard real-time property, multi-perspective and multi-coordinate system observing the scene, and improves the comprehensibility and accuracy of the design.
引用
收藏
页数:7
相关论文
共 50 条
  • [1] Simulation Design of Cyclic Code Error Control System Based on Simulink
    Ma Xiao-qing
    [J]. 2018 INTERNATIONAL CONFERENCE ON SMART GRID AND ELECTRICAL AUTOMATION (ICSGEA), 2018, : 324 - 326
  • [2] Simulink-based simulation platform design and faults impact analysis of attitude control systems
    Song, H.
    Hu, S. L.
    Chen, W. Z.
    [J]. AERONAUTICAL JOURNAL, 2022, 126 (1297): : 475 - 499
  • [3] A comparing design of satellite attitude control system based on reaction wheel
    程颢
    葛升民
    沈毅
    [J]. Journal of Harbin Institute of Technology(New series), 2008, (05) : 638 - 642
  • [4] Research on Modeling and Simulation of Satellite Attitude Control System
    Hu Xiaoguang
    Li Xiang
    [J]. 11TH IEEE INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION (ICCA), 2014, : 744 - 749
  • [5] Design and simulation of fault diagnosis based on NUIO/LMI for satellite attitude control systems
    Cheng, Yuehua
    Hou, Qian
    Jiang, Bin
    [J]. JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2012, 23 (04) : 581 - 587
  • [6] Design of H∞ Controller Based on LMI for Attitude Control System of Flexible Satellite
    Li, Ruixian
    [J]. 2010 INTERNATIONAL CONFERENCE ON INFORMATION, ELECTRONIC AND COMPUTER SCIENCE, VOLS 1-3, 2010, : 2128 - 2131
  • [7] Design and simulation of fault diagnosis based on NUIO/LMI for satellite attitude control systems
    Yuehua Cheng 1
    2. Academy of Frontier Science
    [J]. Journal of Systems Engineering and Electronics, 2012, 23 (04) : 581 - 587
  • [8] Distributed simulation and test of small satellite attitude control system
    Wu Bing
    Liang JiaHong
    Li ShiLei
    Zhang Wenqiong
    [J]. ISTM/2007: 7TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-7, CONFERENCE PROCEEDINGS, 2007, : 5257 - 5260
  • [9] Real-time Simulation System of Satellite Attitude Reconfigurable Control Based on VxWorks
    Ren, Wei
    Zhang, Tao
    Huang, Zhen
    Liang, Jiemei
    Gong, Jian
    Liu, Bo
    [J]. 2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2014, : 2577 - 2580
  • [10] Simulation of Yarn Tension Control System Based on Simulink
    Chang, D. G.
    Xiao, Z. J.
    Liu, Y. H.
    Li, H.
    [J]. FUNCTIONAL MANUFACTURING TECHNOLOGIES AND CEEUSRO I, 2010, 426-427 : 106 - +