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VAN DER LINDEN, S. BOUWMEESTER, J. POVALAČ, A.
Original Title
Design and Validation of an Innovative Data Bus Architecture for CubeSats
Type
abstract
Language
English
Original Abstract
Since the first successful CubeSat missions in the early 2000s, payloads for this form factor have emerged and have increased in technical performance level. This trend is likely to continue in the near future. However, despite the subsequent increase in data load and the increasing modularity of components, there are no clear trends for a new electro-mechanical interface standard. The only widely adopted data bus in CubeSats, I2C, is limited in terms of data rate and reliability. Custom solutions overcoming these limitations are generally not well documented, and especially implementation results in CubeSats are lacking. Therefore, there exists a need to increase the performance and reliability of the CubeSat bus platform. This paper proposes an innovative CubeSat data bus architecture, including performance and reliability tests.
Keywords
CubeSat, data bus, CAN, I2C, USB, RS485
Authors
VAN DER LINDEN, S.; BOUWMEESTER, J.; POVALAČ, A.
Released
27. 10. 2016
Location
London, UK
Pages from
1
Pages to
12
Pages count
BibTex
@misc{BUT129238, author="Stefan {van der Linden} and Jasper {Bouwmeester} and Aleš {Povalač}", title="Design and Validation of an Innovative Data Bus Architecture for CubeSats", booktitle="Proceedings of 14th Reinventing Space Conference, 24-27 October 2016, London, UK.", year="2016", pages="1--12", address="London, UK", note="abstract" }