With the advanced development and maturing of small satellite technologies, there is a high commercial demand for low-cost small satellites with fast delivery for a multitude of applications. This paper presents a hardware-in-the-loop system for testing the satellite's attitude determination and control system and the Agile framework from software engineering practices to guide resource-effective end-to-end development processes, while maintaining a comprehensive system validation. Experimental results for design verification of satellite's Attitude Determination and Control Systems (ADCS) using our ongoing concurrent multiple satellite programs are presented.


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    Titel :

    Agile Development of Small Satellite's Attitude Determination and Control System


    Beteiligte:
    Foo, K.J (Autor:in) / Tissera, M.S.C (Autor:in) / Tan, R.D (Autor:in) / Low, K.S (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    04.03.2023


    Format / Umfang :

    1472333 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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