Software-defined testbed for next generation navigation transponders

Conference Paper (2019)
Author(s)

Stefano Speretta (TU Delft - Aerospace Engineering)

Chris Verhoeven (TU Delft - Electrical Engineering, Mathematics and Computer Science)

Dominic Dirkx (TU Delft - Aerospace Engineering)

Visweswaran Karunanithi (TU Delft - Electrical Engineering, Mathematics and Computer Science)

Mark Bentum (Eindhoven University of Technology)

Odysseas Votsis (Eindhoven University of Technology)

Antonio Miraglia (HKV Lijn in Water - Delft)

Jeroen Rotteveel (HKV Lijn in Water - Delft)

Marco Alvarez (HKV Lijn in Water - Delft)

Hong Yang Oei (HKV Lijn in Water - Delft)

Alberto Busso (European Space Agency (ESA))

Research Group
Space Systems Egineering
DOI related publication
https://doi.org/10.1109/TTC.2019.8895459 Final published version
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Publication Year
2019
Language
English
Research Group
Space Systems Egineering
Bibliographical Note
Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.
Article number
8895459
Publisher
IEEE
ISBN (electronic)
9781728136998
Event
8th ESA International Workshop on Tracking, Telemetry and Command Systems for Space Applications, TTC 2019 (2019-09-24 - 2019-09-27), Darmstadt, Germany
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323
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Abstract

This paper presents a software-defined testbed to perform hardware-in-The-loop test of miniaturized coherent transponders. Such a setup has been designed to minimize the access threshold for future users, heavily relying on available open source applications and commercial hardware, targeting future coherent transponders for interplanetary CubeSats. The paper presents the overall architecture of the testbed, a tradeoff to select the most suited development framework and the detailed design of the different blocks. Upcoming interplanetary CubeSat missions that would require a coherent transponder are also presented to highlight the need sof such a system. Software qualification, given the use of third-party software with multiple developers, was also addressed to guarantee performances can be consistent and reliable.

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