Inter-satellite links for cubesats

Realizing inter-satellite links is a must for ensuring the success of cubesat swarm missions. Nevertheless, it has hardly been considered until now. The communication systems for cubesats have to deal with a few peculiar demands regarding consumed power, geometry and throughput. Depending on the typ...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Budianu, A., Castro, T. J. W., Meijerink, A., Bentum, M. J.
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 10
container_issue
container_start_page 1
container_title
container_volume
creator Budianu, A.
Castro, T. J. W.
Meijerink, A.
Bentum, M. J.
description Realizing inter-satellite links is a must for ensuring the success of cubesat swarm missions. Nevertheless, it has hardly been considered until now. The communication systems for cubesats have to deal with a few peculiar demands regarding consumed power, geometry and throughput. Depending on the type of application, required data rates can go up to tens of megabits per second, while power consumption and physical size are limited by the platform. The proposed communication scheme will combine power-efficient modulation and channel coding with multiple access and spread spectrum techniques, enabling the deployment of multiple satellites. Apart from this, the antenna system has to be designed such that links can be established and maintained independent of the satellites' orientation. An electrically steerable radiation pattern is achieved by placing antennas on each face of the cube. Conformal beamforming provides the system with 5 dBi gain for any desired direction of transmission, eliminating the need for attitude control. Furthermore, using planar antennas reduces the complexity of the mechanical part as they require no deployment.
doi_str_mv 10.1109/AERO.2013.6496947
format Conference Proceeding
fullrecord <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_6496947</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>6496947</ieee_id><sourcerecordid>6496947</sourcerecordid><originalsourceid>FETCH-LOGICAL-i175t-8e5a45bbd40c16fea0198e5aa00346a6fa30dc881968bf3f3fcd10e1b5ea941e3</originalsourceid><addsrcrecordid>eNpVj0tLw0AUhccXGGp-gLgJ7ifeO6_MLEtptVAolAruykxyB0ZjlUxc-O-N2I2cxYHvwAeHsVuEGhHcw3y529YCUNZGOeNUc8ZK11hUppFoEcU5K4Rzhgup7cW_TbhLVkwOzaWQL9eszPkVACatEYgFu18fRxp49iP1fRqp6tPxLVfxY6jar0ATzzfsKvo-U3nqGXteLfeLJ77ZPq4X8w1P2OiRW9Je6RA6BS2aSB7Q_TIPIJXxJnoJXWstOmNDlFPaDoEwaPJOIckZu_vzJiI6fA7p3Q_fh9Nj-QPpGUR-</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Inter-satellite links for cubesats</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Budianu, A. ; Castro, T. J. W. ; Meijerink, A. ; Bentum, M. J.</creator><creatorcontrib>Budianu, A. ; Castro, T. J. W. ; Meijerink, A. ; Bentum, M. J.</creatorcontrib><description>Realizing inter-satellite links is a must for ensuring the success of cubesat swarm missions. Nevertheless, it has hardly been considered until now. The communication systems for cubesats have to deal with a few peculiar demands regarding consumed power, geometry and throughput. Depending on the type of application, required data rates can go up to tens of megabits per second, while power consumption and physical size are limited by the platform. The proposed communication scheme will combine power-efficient modulation and channel coding with multiple access and spread spectrum techniques, enabling the deployment of multiple satellites. Apart from this, the antenna system has to be designed such that links can be established and maintained independent of the satellites' orientation. An electrically steerable radiation pattern is achieved by placing antennas on each face of the cube. Conformal beamforming provides the system with 5 dBi gain for any desired direction of transmission, eliminating the need for attitude control. Furthermore, using planar antennas reduces the complexity of the mechanical part as they require no deployment.</description><identifier>ISSN: 1095-323X</identifier><identifier>ISBN: 9781467318129</identifier><identifier>ISBN: 1467318124</identifier><identifier>EISSN: 2996-2358</identifier><identifier>EISBN: 9781467318112</identifier><identifier>EISBN: 9781467318136</identifier><identifier>EISBN: 1467318132</identifier><identifier>EISBN: 1467318116</identifier><identifier>DOI: 10.1109/AERO.2013.6496947</identifier><language>eng</language><publisher>IEEE</publisher><subject>Antenna radiation patterns ; Bit error rate ; Gain ; Noise ; Satellite broadcasting ; Satellites</subject><ispartof>2013 IEEE Aerospace Conference, 2013, p.1-10</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/6496947$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2051,27904,54898</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/6496947$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Budianu, A.</creatorcontrib><creatorcontrib>Castro, T. J. W.</creatorcontrib><creatorcontrib>Meijerink, A.</creatorcontrib><creatorcontrib>Bentum, M. J.</creatorcontrib><title>Inter-satellite links for cubesats</title><title>2013 IEEE Aerospace Conference</title><addtitle>AERO</addtitle><description>Realizing inter-satellite links is a must for ensuring the success of cubesat swarm missions. Nevertheless, it has hardly been considered until now. The communication systems for cubesats have to deal with a few peculiar demands regarding consumed power, geometry and throughput. Depending on the type of application, required data rates can go up to tens of megabits per second, while power consumption and physical size are limited by the platform. The proposed communication scheme will combine power-efficient modulation and channel coding with multiple access and spread spectrum techniques, enabling the deployment of multiple satellites. Apart from this, the antenna system has to be designed such that links can be established and maintained independent of the satellites' orientation. An electrically steerable radiation pattern is achieved by placing antennas on each face of the cube. Conformal beamforming provides the system with 5 dBi gain for any desired direction of transmission, eliminating the need for attitude control. Furthermore, using planar antennas reduces the complexity of the mechanical part as they require no deployment.</description><subject>Antenna radiation patterns</subject><subject>Bit error rate</subject><subject>Gain</subject><subject>Noise</subject><subject>Satellite broadcasting</subject><subject>Satellites</subject><issn>1095-323X</issn><issn>2996-2358</issn><isbn>9781467318129</isbn><isbn>1467318124</isbn><isbn>9781467318112</isbn><isbn>9781467318136</isbn><isbn>1467318132</isbn><isbn>1467318116</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2013</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNpVj0tLw0AUhccXGGp-gLgJ7ifeO6_MLEtptVAolAruykxyB0ZjlUxc-O-N2I2cxYHvwAeHsVuEGhHcw3y529YCUNZGOeNUc8ZK11hUppFoEcU5K4Rzhgup7cW_TbhLVkwOzaWQL9eszPkVACatEYgFu18fRxp49iP1fRqp6tPxLVfxY6jar0ATzzfsKvo-U3nqGXteLfeLJ77ZPq4X8w1P2OiRW9Je6RA6BS2aSB7Q_TIPIJXxJnoJXWstOmNDlFPaDoEwaPJOIckZu_vzJiI6fA7p3Q_fh9Nj-QPpGUR-</recordid><startdate>201303</startdate><enddate>201303</enddate><creator>Budianu, A.</creator><creator>Castro, T. J. W.</creator><creator>Meijerink, A.</creator><creator>Bentum, M. J.</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>201303</creationdate><title>Inter-satellite links for cubesats</title><author>Budianu, A. ; Castro, T. J. W. ; Meijerink, A. ; Bentum, M. J.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i175t-8e5a45bbd40c16fea0198e5aa00346a6fa30dc881968bf3f3fcd10e1b5ea941e3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Antenna radiation patterns</topic><topic>Bit error rate</topic><topic>Gain</topic><topic>Noise</topic><topic>Satellite broadcasting</topic><topic>Satellites</topic><toplevel>online_resources</toplevel><creatorcontrib>Budianu, A.</creatorcontrib><creatorcontrib>Castro, T. J. W.</creatorcontrib><creatorcontrib>Meijerink, A.</creatorcontrib><creatorcontrib>Bentum, M. J.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Xplore</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Budianu, A.</au><au>Castro, T. J. W.</au><au>Meijerink, A.</au><au>Bentum, M. J.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Inter-satellite links for cubesats</atitle><btitle>2013 IEEE Aerospace Conference</btitle><stitle>AERO</stitle><date>2013-03</date><risdate>2013</risdate><spage>1</spage><epage>10</epage><pages>1-10</pages><issn>1095-323X</issn><eissn>2996-2358</eissn><isbn>9781467318129</isbn><isbn>1467318124</isbn><eisbn>9781467318112</eisbn><eisbn>9781467318136</eisbn><eisbn>1467318132</eisbn><eisbn>1467318116</eisbn><abstract>Realizing inter-satellite links is a must for ensuring the success of cubesat swarm missions. Nevertheless, it has hardly been considered until now. The communication systems for cubesats have to deal with a few peculiar demands regarding consumed power, geometry and throughput. Depending on the type of application, required data rates can go up to tens of megabits per second, while power consumption and physical size are limited by the platform. The proposed communication scheme will combine power-efficient modulation and channel coding with multiple access and spread spectrum techniques, enabling the deployment of multiple satellites. Apart from this, the antenna system has to be designed such that links can be established and maintained independent of the satellites' orientation. An electrically steerable radiation pattern is achieved by placing antennas on each face of the cube. Conformal beamforming provides the system with 5 dBi gain for any desired direction of transmission, eliminating the need for attitude control. Furthermore, using planar antennas reduces the complexity of the mechanical part as they require no deployment.</abstract><pub>IEEE</pub><doi>10.1109/AERO.2013.6496947</doi><tpages>10</tpages></addata></record>
fulltext fulltext_linktorsrc
identifier ISSN: 1095-323X
ispartof 2013 IEEE Aerospace Conference, 2013, p.1-10
issn 1095-323X
2996-2358
language eng
recordid cdi_ieee_primary_6496947
source IEEE Electronic Library (IEL) Conference Proceedings
subjects Antenna radiation patterns
Bit error rate
Gain
Noise
Satellite broadcasting
Satellites
title Inter-satellite links for cubesats
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-24T17%3A59%3A07IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-ieee_6IE&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Inter-satellite%20links%20for%20cubesats&rft.btitle=2013%20IEEE%20Aerospace%20Conference&rft.au=Budianu,%20A.&rft.date=2013-03&rft.spage=1&rft.epage=10&rft.pages=1-10&rft.issn=1095-323X&rft.eissn=2996-2358&rft.isbn=9781467318129&rft.isbn_list=1467318124&rft_id=info:doi/10.1109/AERO.2013.6496947&rft_dat=%3Cieee_6IE%3E6496947%3C/ieee_6IE%3E%3Curl%3E%3C/url%3E&rft.eisbn=9781467318112&rft.eisbn_list=9781467318136&rft.eisbn_list=1467318132&rft.eisbn_list=1467318116&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=6496947&rfr_iscdi=true