This paper describes the hardware-in-the-loop (HIL) simulation methodology used for the verification of functional requirements of e-st @r-I CubeSat. The satellite's behavior is investigated via HIL simulation, and the results obtained are consistent with the expected values in any operative conditions. It is proven that HIL simulation is a valuable means for supporting the verification process of small satellites and may help reduce the time and cost of the development phase and increase mission reliability.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Verification of a CubeSat via hardware-in-the-loop simulation


    Contributors:


    Publication date :

    2014-10-01


    Size :

    1559991 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Hardware-In-The-Loop experiments of an attitude fusing library for CubeSat star trackers

    Samson, Mikel R. / Kazemi, Laila / Van de Putte, Rhimas et al. | AIAA | 2024


    Testing the attitude determination and control of a CubeSat with hardware-in-the-loop

    Quadrino, Meghan Kathleen | DSpace@MIT | 2014

    Free access

    Finding life on Mars using CubeSat hardware??

    McCormick, Ryan L. / Castano, Rebecca / Stricker, Moogega C. et al. | NTRS | 2018


    CubeSat Autonomous Rendezvous Simulation

    Lightsey, E Glenn / Fear, Andrew J. | AIAA | 2015