• DocumentCode
    1775437
  • Title

    Research on modeling and simulation of satellite attitude control system

  • Author

    Xiaoguang Hu ; Xiang Li

  • Author_Institution
    Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
  • fYear
    2014
  • fDate
    18-20 June 2014
  • Firstpage
    744
  • Lastpage
    749
  • Abstract
    Satellite is a specific product with a 4-H characteristic: high-tech, high-cost, high-benefit and high-risk, which makes satellite difficult to develop. However, simulation technology has the potential to fix the problem. It is highly reliable, non-destructive and can be recycled regardless of the time and space. All the advantages enable the technology to provide an effective way to reduce the cost and risk of satellite production. The paper focuses on the modeling technology which is used for simulating satellite on-orbit performance and dynamic environment, thus it can provide a general simulation framework for test during the development of a satellite.
  • Keywords
    aerospace simulation; artificial satellites; attitude control; cost reduction; risk management; vehicle dynamics; control system modeling; control system simulation; cost reduction; dynamic environment; modeling technology; risk reduction; satellite attitude control system; satellite development; satellite on-orbit performance simulation; satellite production; simulation technology; Attitude control; Equations; Mathematical model; Position measurement; Satellites; Sensors; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control & Automation (ICCA), 11th IEEE International Conference on
  • Conference_Location
    Taichung
  • Type

    conf

  • DOI
    10.1109/ICCA.2014.6871014
  • Filename
    6871014