• DocumentCode
    3042208
  • Title

    A real-time simulation system for satellite based on RTW and VxWorks

  • Author

    Shen, Erjian ; Zhang, Tao ; Huang, Liangwei ; Liang, Bin ; Song, Jingyan

  • Author_Institution
    Dept. of Autom., Tsinghua Univ., Beijing, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    859
  • Lastpage
    864
  • Abstract
    A new real-time simulation system is developed based on the Real Time Workshop (RTW) and real-time operation system VxWorks. The whole model of satellite is defined, which is proved by simulation in Simulink. This model is divided into two parts. One part is the attitude and orbit controller, i.e., attitude and orbit control system (AOCS), named AOCS model. The other is the external model of AOCS, named external model. The CAN bus interface blocks are designed for the two parts, respectively. The compiled codes of the two models are downloaded to two target computers with VxWorks for real-time simulation, which are connected by CAN bus. In addition, a method is proposed to verify the availability of the model in VxWorks, although not all blocks in Simulink can be implemented in VxWorks. This proposed method is compared by the simulation results of simulation in the Simulink and VxWorks. A simulation example is developed to test the availability and reliability of the system.
  • Keywords
    aerospace computing; aerospace simulation; controller area networks; operating systems (computers); real-time systems; AOCS external model; AOCS model; CAN bus interface; RTW; Simulink; attitude controller; orbit control system; orbit controller; real time workshop; real-time operation system VxWorks; real-time simulation system; satellite; system reliability; Computational modeling; Computers; Data models; Mathematical model; Real time systems; Satellites; Sun;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5633094
  • Filename
    5633094