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.


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    Titel :

    PolySat's Next Generation Avionics Design


    Beteiligte:
    Manyak, G. (Autor:in) / Bellardo, J. M. (Autor:in)


    Erscheinungsdatum :

    01.08.2011


    Format / Umfang :

    811915 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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