American Journal of Applied Scientific Research

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A Reconfigurable Hybrid Digital Processor for Dual Use Advanced Satellite Communication Missions

Received: 10 November 2018    Accepted: 03 December 2018    Published: 07 January 2019
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Abstract

The continuous evolution of the air interfaces during the satellite lifetime, the risk of a rapid obsolescence of a payload based on on-board processing capabilities are suggesting more and more the adoption of Reconfigurable Software Radio techniques, which can be exploited to adapt the on-board processor to new waveforms, implementing software defined payload configurations; at this aim the current work proposes a new Hybrid Regenerative and Transparent Digital Processor architecture in order to improve the system flexibility and support dual-use satellite missions for civil and military applications, and finally presents some experimental results achieved in a representative end-to-end testbed demonstrator, integrating the Reconfigurable Hybrid Digital Processor.

DOI 10.11648/j.ajasr.20180404.11
Published in American Journal of Applied Scientific Research (Volume 4, Issue 4, December 2018)
Page(s) 41-51
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2024. Published by Science Publishing Group

Keywords

SatCom, Reconfigurable Software Defined, Reconfigurable Hybrid Digital Processor, Dual-Use, OBP

References
[1] NC3A, AC/322 (SC/6) N (2008) 0015, NATO Network Enabled Capability Feasibility Study Executive Summary, Issue 2
[2] NC3A, AC/322 (SC/6-WG/1) N (2008) 0006, AC/322 (SC/6) N (2008) 0010, NII Communications Reference Architecture, Issue 1.1
[3] NC3A, AC/322 (SC/6-WG/2) N (2008) 0005, NATO SATCOM Ground Reference Architecture, Issue 2
[4] GINS/D023/TPZ/TN/023 GINS Feasibility Study: Final Report, Telespazio, Thales Alenia Space, TNO
[5] IEEE P1900.1 - Draft Standard Definitions and Concepts for Dynamic Spectrum Access-Terminology Relating to Emerging Wireless Networks, System Functionality, and Spectrum Management
[6] P. Angeletti, R. De Gaudenzi, M. Lisi, From "Bent Pipes" to "Software Defined Payloads": Evolution and Trends of Satellite Communications Systems, DOI: 10.2514/6.2008-5439, 06/2008.
[7] T. C. Butash, J. R. Marshall, Leveraging Digital On-Board Processing to Increase Communications Satellite Flexibility and Effective Capacity, 28th AIAA Conference (ICSSC-2010), 9/2010
[8] A. W. Mast, Reconfigurable Software Defined Payload Architecture That Reduces Cost and Risk for Various Missions, IEEE 978-1-4244-7351-9/11, 2011
[9] G. Allen, L. Edmonds, C. W. Tseng, G. Swift, and C. Carmichael., “Single-Event Upset (SEU) Results of Embedded Error Detect and Correct Enabled Block Random Access Memory (Block RAM) within the Xilinx XQR5VFX130” 2010 Radiation Effects Data Workshop Record, (http://parts.jpl.nasa.gov/wp-content/uploads/EDACfinal-IEEE-proof.pdf)
[10] F. Iacomacci, C. Morlet, F. Autelitano, G. C. Cardarilli, M. Re, E. Petrongari, G. Bogo, M. Francescheli, A Software Defined Radio Architecture for a Regenerative On-Board Processor, Proceedings of AHS. 2008.
[11] G. Tomasicchio, A. Pisano, D. Giancristofaro, “New Satcoms Architectures with Reconfigurable Digital On Board Processing Technologies”, Proceedings of the 2nd ESA Workshop on Advanced Flexible Telecom Payloads, Noordwijk, The Netherlands; 04/2012; ESA.
[12] G. Lulli, F. Iacomacci, G. Losquadro, G. Tomasicchio, Software Radio for OBP Systems Implementations: Architecture and Technology for a Reconfigurable Platform, 19th Ka and Broadband Communications Conference, 10/2013.
[13] G. Pastore, G. Losquadro, G. Tomasicchio, G. Belvedere, TCol. L. Mauro, A “Software Defined Payload” for dual use satellite systems, 21th Ka and Broadband Communications Conference, Bologna, Italy, October 2015.
[14] G. Pastore, G. Losquadro, G. Lulli, G. Tomasicchio, A “Software Defined Payload” for Dual Use Satellite System Architectures”, Presented at 3rd ESA Workshop on Advanced Flexible Telecom Payloads, ESTEC, Noordwijk, The Netherlands, March 2016.
[15] G. Tomasicchio, G. Pastore, G. Lulli, D. Giancristofaro, C. Moca, Hybrid OBP with DBAC-based Switching Control for Multi-Beam Satellite Systems (Submitted as Thales Alenia Space Italia company). Patent Pending No. registration: PCT/EP2017/058471.
Author Information
  • Domain Observation and Navigation Italy, Thales Alenia Space Italia, Rome, Italy

  • Domain Observation and Navigation Italy, Thales Alenia Space Italia, Rome, Italy

  • Domain Observation and Navigation Italy, Thales Alenia Space Italia, Rome, Italy

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  • APA Style

    Giuseppe Tomasicchio, Guglielmo Lulli, Gaetano Pastore. (2019). A Reconfigurable Hybrid Digital Processor for Dual Use Advanced Satellite Communication Missions. American Journal of Applied Scientific Research, 4(4), 41-51. https://doi.org/10.11648/j.ajasr.20180404.11

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    ACS Style

    Giuseppe Tomasicchio; Guglielmo Lulli; Gaetano Pastore. A Reconfigurable Hybrid Digital Processor for Dual Use Advanced Satellite Communication Missions. Am. J. Appl. Sci. Res. 2019, 4(4), 41-51. doi: 10.11648/j.ajasr.20180404.11

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    AMA Style

    Giuseppe Tomasicchio, Guglielmo Lulli, Gaetano Pastore. A Reconfigurable Hybrid Digital Processor for Dual Use Advanced Satellite Communication Missions. Am J Appl Sci Res. 2019;4(4):41-51. doi: 10.11648/j.ajasr.20180404.11

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  • @article{10.11648/j.ajasr.20180404.11,
      author = {Giuseppe Tomasicchio and Guglielmo Lulli and Gaetano Pastore},
      title = {A Reconfigurable Hybrid Digital Processor for Dual Use Advanced Satellite Communication Missions},
      journal = {American Journal of Applied Scientific Research},
      volume = {4},
      number = {4},
      pages = {41-51},
      doi = {10.11648/j.ajasr.20180404.11},
      url = {https://doi.org/10.11648/j.ajasr.20180404.11},
      eprint = {https://download.sciencepg.com/pdf/10.11648.j.ajasr.20180404.11},
      abstract = {The continuous evolution of the air interfaces during the satellite lifetime, the risk of a rapid obsolescence of a payload based on on-board processing capabilities are suggesting more and more the adoption of Reconfigurable Software Radio techniques, which can be exploited to adapt the on-board processor to new waveforms, implementing software defined payload configurations; at this aim the current work proposes a new Hybrid Regenerative and Transparent Digital Processor architecture in order to improve the system flexibility and support dual-use satellite missions for civil and military applications, and finally presents some experimental results achieved in a representative end-to-end testbed demonstrator, integrating the Reconfigurable Hybrid Digital Processor.},
     year = {2019}
    }
    

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    T1  - A Reconfigurable Hybrid Digital Processor for Dual Use Advanced Satellite Communication Missions
    AU  - Giuseppe Tomasicchio
    AU  - Guglielmo Lulli
    AU  - Gaetano Pastore
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    JO  - American Journal of Applied Scientific Research
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    EP  - 51
    PB  - Science Publishing Group
    SN  - 2471-9730
    UR  - https://doi.org/10.11648/j.ajasr.20180404.11
    AB  - The continuous evolution of the air interfaces during the satellite lifetime, the risk of a rapid obsolescence of a payload based on on-board processing capabilities are suggesting more and more the adoption of Reconfigurable Software Radio techniques, which can be exploited to adapt the on-board processor to new waveforms, implementing software defined payload configurations; at this aim the current work proposes a new Hybrid Regenerative and Transparent Digital Processor architecture in order to improve the system flexibility and support dual-use satellite missions for civil and military applications, and finally presents some experimental results achieved in a representative end-to-end testbed demonstrator, integrating the Reconfigurable Hybrid Digital Processor.
    VL  - 4
    IS  - 4
    ER  - 

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