Design of a dual-antenna and dual-band GPS receiver for CubeSats
- Autores
- Rodríguez, Santiago; López La Valle, Ramón Gerardo; Puga, Gerardo Ludovico; García, Javier Gonzalo; Roncagliolo, Pedro Agustín
- Año de publicación
- 2017
- Idioma
- español castellano
- Tipo de recurso
- documento de conferencia
- Estado
- versión publicada
- Descripción
- During the last few years, there has been a rise in the use of nanosatellites because they offer a low cost and short development time alternative to larger satellites intended for longduration missions. The use of commercial components (COTS) instead of the expensive space-grade components required for long missions is one of the main reasons of the popularity of the nanosatellites. This paper presents the hardware design of a GPS receiver compatible with the CubeSat standard. The receiver has two antenna inputs and is capable of operating on the L1 and L2 bands. Since the proposed design is based on non-space qualified components, a tolerance and fault mitigation scheme for SEU and SEL events produced by the effect of radiation is implemented.
Facultad de Ingeniería - Materia
-
Ingeniería
Artificial satellites
Global Positioning System
Radio receivers
Satellite antennas - Nivel de accesibilidad
- acceso abierto
- Condiciones de uso
- http://creativecommons.org/licenses/by-nc-sa/4.0/
- Repositorio
- Institución
- Universidad Nacional de La Plata
- OAI Identificador
- oai:sedici.unlp.edu.ar:10915/154329
Ver los metadatos del registro completo
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Design of a dual-antenna and dual-band GPS receiver for CubeSatsRodríguez, SantiagoLópez La Valle, Ramón GerardoPuga, Gerardo LudovicoGarcía, Javier GonzaloRoncagliolo, Pedro AgustínIngenieríaArtificial satellitesGlobal Positioning SystemRadio receiversSatellite antennasDuring the last few years, there has been a rise in the use of nanosatellites because they offer a low cost and short development time alternative to larger satellites intended for longduration missions. The use of commercial components (COTS) instead of the expensive space-grade components required for long missions is one of the main reasons of the popularity of the nanosatellites. This paper presents the hardware design of a GPS receiver compatible with the CubeSat standard. The receiver has two antenna inputs and is capable of operating on the L1 and L2 bands. Since the proposed design is based on non-space qualified components, a tolerance and fault mitigation scheme for SEU and SEL events produced by the effect of radiation is implemented.Facultad de Ingeniería2017-10info:eu-repo/semantics/conferenceObjectinfo:eu-repo/semantics/publishedVersionObjeto de conferenciahttp://purl.org/coar/resource_type/c_5794info:ar-repo/semantics/documentoDeConferenciaapplication/pdfhttp://sedici.unlp.edu.ar/handle/10915/154329spainfo:eu-repo/semantics/altIdentifier/isbn/978-1-5386-3397-7info:eu-repo/semantics/altIdentifier/doi/10.1109/URUCON.2017.8171862info:eu-repo/semantics/openAccesshttp://creativecommons.org/licenses/by-nc-sa/4.0/Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)reponame:SEDICI (UNLP)instname:Universidad Nacional de La Platainstacron:UNLP2025-09-03T11:11:57Zoai:sedici.unlp.edu.ar:10915/154329Institucionalhttp://sedici.unlp.edu.ar/Universidad públicaNo correspondehttp://sedici.unlp.edu.ar/oai/snrdalira@sedici.unlp.edu.arArgentinaNo correspondeNo correspondeNo correspondeopendoar:13292025-09-03 11:11:58.107SEDICI (UNLP) - Universidad Nacional de La Platafalse |
dc.title.none.fl_str_mv |
Design of a dual-antenna and dual-band GPS receiver for CubeSats |
title |
Design of a dual-antenna and dual-band GPS receiver for CubeSats |
spellingShingle |
Design of a dual-antenna and dual-band GPS receiver for CubeSats Rodríguez, Santiago Ingeniería Artificial satellites Global Positioning System Radio receivers Satellite antennas |
title_short |
Design of a dual-antenna and dual-band GPS receiver for CubeSats |
title_full |
Design of a dual-antenna and dual-band GPS receiver for CubeSats |
title_fullStr |
Design of a dual-antenna and dual-band GPS receiver for CubeSats |
title_full_unstemmed |
Design of a dual-antenna and dual-band GPS receiver for CubeSats |
title_sort |
Design of a dual-antenna and dual-band GPS receiver for CubeSats |
dc.creator.none.fl_str_mv |
Rodríguez, Santiago López La Valle, Ramón Gerardo Puga, Gerardo Ludovico García, Javier Gonzalo Roncagliolo, Pedro Agustín |
author |
Rodríguez, Santiago |
author_facet |
Rodríguez, Santiago López La Valle, Ramón Gerardo Puga, Gerardo Ludovico García, Javier Gonzalo Roncagliolo, Pedro Agustín |
author_role |
author |
author2 |
López La Valle, Ramón Gerardo Puga, Gerardo Ludovico García, Javier Gonzalo Roncagliolo, Pedro Agustín |
author2_role |
author author author author |
dc.subject.none.fl_str_mv |
Ingeniería Artificial satellites Global Positioning System Radio receivers Satellite antennas |
topic |
Ingeniería Artificial satellites Global Positioning System Radio receivers Satellite antennas |
dc.description.none.fl_txt_mv |
During the last few years, there has been a rise in the use of nanosatellites because they offer a low cost and short development time alternative to larger satellites intended for longduration missions. The use of commercial components (COTS) instead of the expensive space-grade components required for long missions is one of the main reasons of the popularity of the nanosatellites. This paper presents the hardware design of a GPS receiver compatible with the CubeSat standard. The receiver has two antenna inputs and is capable of operating on the L1 and L2 bands. Since the proposed design is based on non-space qualified components, a tolerance and fault mitigation scheme for SEU and SEL events produced by the effect of radiation is implemented. Facultad de Ingeniería |
description |
During the last few years, there has been a rise in the use of nanosatellites because they offer a low cost and short development time alternative to larger satellites intended for longduration missions. The use of commercial components (COTS) instead of the expensive space-grade components required for long missions is one of the main reasons of the popularity of the nanosatellites. This paper presents the hardware design of a GPS receiver compatible with the CubeSat standard. The receiver has two antenna inputs and is capable of operating on the L1 and L2 bands. Since the proposed design is based on non-space qualified components, a tolerance and fault mitigation scheme for SEU and SEL events produced by the effect of radiation is implemented. |
publishDate |
2017 |
dc.date.none.fl_str_mv |
2017-10 |
dc.type.none.fl_str_mv |
info:eu-repo/semantics/conferenceObject info:eu-repo/semantics/publishedVersion Objeto de conferencia http://purl.org/coar/resource_type/c_5794 info:ar-repo/semantics/documentoDeConferencia |
format |
conferenceObject |
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publishedVersion |
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http://sedici.unlp.edu.ar/handle/10915/154329 |
url |
http://sedici.unlp.edu.ar/handle/10915/154329 |
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info:eu-repo/semantics/altIdentifier/isbn/978-1-5386-3397-7 info:eu-repo/semantics/altIdentifier/doi/10.1109/URUCON.2017.8171862 |
dc.rights.none.fl_str_mv |
info:eu-repo/semantics/openAccess http://creativecommons.org/licenses/by-nc-sa/4.0/ Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0) |
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http://creativecommons.org/licenses/by-nc-sa/4.0/ Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0) |
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