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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    Title :

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


    Contributors:
    Foo, K.J (author) / Tissera, M.S.C (author) / Tan, R.D (author) / Low, K.S (author)


    Publication date :

    2023-03-04


    Size :

    1472333 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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