Abstract

Design and verification techniques targeting the space environment, are widely used to explore reliability levels of embedded systems for Cubesats. Considering that, we carried out a study to select and to adapt a design flow to be used as a guide for the development of Cubesats. The chosen design and development flow was used in a case study of a board, called Payload-XL, conceived to be the computing module of a Cubesat. The primary purpose of Payload-XL is to validate the BRAVE FPGA from Nanoxplore, in orbit. Research and development activities were carried out to integrate the GOMX-5 mission through a partnership between the Federal University of Santa Catarina, the European Space Agency, Cobham Gaisler, GMV, CBK, and GomSpace. The results demonstrate that Payload-XL innovates as a validation platform for the BRAVE FPGA, and also bringing mechanisms to reconfigure it remotely in orbit. Furthermore, the results show that Payload-XL complies with the power, size, and requirements of the GOMX-5 mission.

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