CubeSat attitude control systems must be compact, fast, and accurate to achieve success in space missions with stringent control requirements. Nonlinear control strategies allow the creation of robust algorithms for orbit and attitude control, but can have higher processing requirements for effective operation. In addition, It is desirable to distribute components of a CubeSat control system across hardware as much as possible to decrease the load on a central computing unit and to make the system more tolerant to point failures. Field Programmable Gate Array technology has become a popular solution to the limited electronic space and demanding processing requirements present in new-generation CubeSat systems. This paper will focus on demonstrating the feasibility and effectiveness of a proposed nonlinear adaptive fuzzy controller implemented on a Field Programmable Gate Array as part of a highly-integrated space hardware system that is under development.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    FPGA hardware nonlinear control design for modular CubeSat attitude control system


    Beteiligte:
    Li, Junquan (Autor:in) / Post, Mark (Autor:in) / Lee, Regina (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2015-03-01


    Format / Umfang :

    3857661 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    CubeSat Attitude Control Simulator Design

    Thomas, Dylan / Wolosik, Anthony T. / Black, Jonathan | AIAA | 2018


    Cubesat Solar Sail Attitude Determination and Control System Hardware Design and Orbital Analysis

    Lappas, Vaios / Adeli, Nasir / Bisagie, Lourens et al. | AIAA | 2010


    Cubesat Solar Sail Attitude Determination and Control System Hardware Design and Orbital Analysis

    Lappas, V. / Adeli, N. / Visagie, L. et al. | British Library Conference Proceedings | 2010


    Magnetic-based Attitude Control scheme for CubeSat

    Xia, Xiwang / Wu, Shufan / Sun, Guowen et al. | IEEE | 2016


    Novel attitude control devices for CubeSat satellites

    Bručas, Domantas / Bansevičius, Ramutis / Domeika, Aurelijus et al. | BASE | 2012

    Freier Zugriff