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.
Agile Development of Small Satellite's Attitude Determination and Control System
04.03.2023
1472333 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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