• DocumentCode
    3125892
  • Title

    PolySat´s Next Generation Avionics Design

  • Author

    Manyak, Greg ; Bellardo, John M.

  • Author_Institution
    Electr. Eng. Dept., California Polytech. State Univ., San Luis Obispo, CA, USA
  • fYear
    2011
  • fDate
    2-4 Aug. 2011
  • Firstpage
    69
  • Lastpage
    76
  • Abstract
    The CubeSat platform provides a unique challenge for flight software design due to the incredible size and power constraints. A number of tradeoffs must be made to balance effectiveness, fault tolerance, and cost. These basic requirements have been combined with the lessons learned from Cal Poly´s past 8-bit avionics system to design a significant revision based around a 32-bit microprocessor running Linux. This work analyzes both generations of avionics design, including a discussion of major design principles that are relevant to other CubeSat missions.
  • Keywords
    Linux; aerospace computing; artificial satellites; avionics; microprocessor chips; software fault tolerance; CubeSat missions; CubeSat platform; Linux; PolySat next generation avionic design; fault tolerance; flight software design; microprocessor; word length 32 bit; Aerospace electronics; Batteries; Fault tolerance; Hardware; Payloads; Satellites; Software; cubesat software design; fault tolerance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Space Mission Challenges for Information Technology (SMC-IT), 2011 IEEE Fourth International Conference on
  • Conference_Location
    Palo Alto, CA
  • Print_ISBN
    978-1-4577-0712-4
  • Electronic_ISBN
    978-1-4577-0713-1
  • Type

    conf

  • DOI
    10.1109/SMC-IT.2011.13
  • Filename
    6007777