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A high-performance computing module for a low earth orbit satellite using reconfigurable logic

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Part of the book series: Lecture Notes in Computer Science ((LNCS,volume 1482))

Abstract

A hierarchy of FPGAs, DSPs, and a multiprocessing microprocessor provide a layered high performance computing module which will be used to enhance the performance of a low-earth orbit satellite, FedSat-1, which will be operational in 2001. The high performance computer will provide additional hardware redundancy, on-board data processing, data filtering and data compression for science data, as well as allowing experiments in dynamic reconfigurability of satellite computing hardware in space.

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References

  1. Kingwell, J., Embleton, B.: Cooperative Research Centre for Satellite Systems, World Wide Web page at http://www.crcss.csiro.au/, (1998)

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  2. Jilla, C. D., Miller, D. W.: Satellite Design: Past, Present and Future, International Journal of Small Satellite Engineering, Vol. 1, No. 1, (1995) World Wide Web page at http://www.ee.surrey.ac.uk/EE/CSER/UOSAT/IJSSE/issue1/cjilla/cjilla.html

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  3. Wagner, D.J.: Spaceborne Processors: Past, Present and Future Satellite Onboard Computers, Proceedings of 49th International Astronautical Federation Congress, Melbourne (1998)

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Reiner W. Hartenstein Andres Keevallik

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© 1998 Springer-Verlag Berlin Heidelberg

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Bergmann, N.W., Sutton, P.R. (1998). A high-performance computing module for a low earth orbit satellite using reconfigurable logic. In: Hartenstein, R.W., Keevallik, A. (eds) Field-Programmable Logic and Applications From FPGAs to Computing Paradigm. FPL 1998. Lecture Notes in Computer Science, vol 1482. Springer, Berlin, Heidelberg. https://doi.org/10.1007/BFb0055272

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  • DOI: https://doi.org/10.1007/BFb0055272

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-64948-9

  • Online ISBN: 978-3-540-68066-6

  • eBook Packages: Springer Book Archive

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