Electrical interfaces compatibility analysis for the COMS EPS
The COMS (communication, ocean and meteorological satellite) EPS (electrical power subsystem) is derived from an enhanced Eurostar 3000. The COMS EPS can offer a bus power capability of 3 kW. The aim of this analysis is to verify the electrical compatibility of the interfaces which exist between COM...
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creator | Ja-Chun Koo Eui-Chan Kim |
description | The COMS (communication, ocean and meteorological satellite) EPS (electrical power subsystem) is derived from an enhanced Eurostar 3000. The COMS EPS can offer a bus power capability of 3 kW. The aim of this analysis is to verify the electrical compatibility of the interfaces which exist between COMS EPS equipments and external equipments. For each interface, this study checked the compatibility between equipments for the power links, commands, digital telemetry, analog telemetry and failure condition. In addition with this interface compatibility verification, this study outputs electrical and manufacturing constraints to be applied at harness level. |
doi_str_mv | 10.1109/ICPE.2007.4692402 |
format | Conference Proceeding |
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The COMS EPS can offer a bus power capability of 3 kW. The aim of this analysis is to verify the electrical compatibility of the interfaces which exist between COMS EPS equipments and external equipments. For each interface, this study checked the compatibility between equipments for the power links, commands, digital telemetry, analog telemetry and failure condition. In addition with this interface compatibility verification, this study outputs electrical and manufacturing constraints to be applied at harness level.</description><identifier>ISSN: 2150-6078</identifier><identifier>ISBN: 9781424418718</identifier><identifier>ISBN: 1424418712</identifier><identifier>EISBN: 9781424418725</identifier><identifier>EISBN: 1424418720</identifier><identifier>DOI: 10.1109/ICPE.2007.4692402</identifier><language>eng</language><publisher>IEEE</publisher><subject>Aerospace electronics ; Batteries ; Frequency ; Fuses ; Manufacturing ; Performance analysis ; Power electronics ; Telemetry ; Voltage ; Wires</subject><ispartof>2007 7th Internatonal Conference on Power Electronics, 2007, p.324-329</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/4692402$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2052,27902,54895</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/4692402$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Ja-Chun Koo</creatorcontrib><creatorcontrib>Eui-Chan Kim</creatorcontrib><title>Electrical interfaces compatibility analysis for the COMS EPS</title><title>2007 7th Internatonal Conference on Power Electronics</title><addtitle>ICPE</addtitle><description>The COMS (communication, ocean and meteorological satellite) EPS (electrical power subsystem) is derived from an enhanced Eurostar 3000. The COMS EPS can offer a bus power capability of 3 kW. The aim of this analysis is to verify the electrical compatibility of the interfaces which exist between COMS EPS equipments and external equipments. For each interface, this study checked the compatibility between equipments for the power links, commands, digital telemetry, analog telemetry and failure condition. In addition with this interface compatibility verification, this study outputs electrical and manufacturing constraints to be applied at harness level.</description><subject>Aerospace electronics</subject><subject>Batteries</subject><subject>Frequency</subject><subject>Fuses</subject><subject>Manufacturing</subject><subject>Performance analysis</subject><subject>Power electronics</subject><subject>Telemetry</subject><subject>Voltage</subject><subject>Wires</subject><issn>2150-6078</issn><isbn>9781424418718</isbn><isbn>1424418712</isbn><isbn>9781424418725</isbn><isbn>1424418720</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2007</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNpVj8tKAzEYhSMqWOo8gLjJC8z4554sXMgwaqHSQrsvf2YSjEwvTLLp21uwG1eH8y3OxyHkiUHDGLiXRbvuGg5gGqkdl8BvSOWMZZJLyazh6vZfZ_aOzDhTUGsw9oFUOf8AAHPaSGdn5LUbQ1-m1ONI06GEKWIfMu2P-xOW5NOYypniAcdzTpnG40TLd6Dt6mtDu_XmkdxHHHOorjkn2_du237Wy9XHon1b1slBqXlUOHC8-J3yEr3wNkYvhoGDESxoCMILPYQeZbRSmQuOimtmAbUBb8ScPP_NphDC7jSlPU7n3fW_-AUf4UsD</recordid><startdate>200710</startdate><enddate>200710</enddate><creator>Ja-Chun Koo</creator><creator>Eui-Chan Kim</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>200710</creationdate><title>Electrical interfaces compatibility analysis for the COMS EPS</title><author>Ja-Chun Koo ; Eui-Chan Kim</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i90t-2f5ad2a07895b4ab3b8ffb3dd20731e60e3b36deca4f8457207f526180a670b73</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2007</creationdate><topic>Aerospace electronics</topic><topic>Batteries</topic><topic>Frequency</topic><topic>Fuses</topic><topic>Manufacturing</topic><topic>Performance analysis</topic><topic>Power electronics</topic><topic>Telemetry</topic><topic>Voltage</topic><topic>Wires</topic><toplevel>online_resources</toplevel><creatorcontrib>Ja-Chun Koo</creatorcontrib><creatorcontrib>Eui-Chan Kim</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</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>Ja-Chun Koo</au><au>Eui-Chan Kim</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Electrical interfaces compatibility analysis for the COMS EPS</atitle><btitle>2007 7th Internatonal Conference on Power Electronics</btitle><stitle>ICPE</stitle><date>2007-10</date><risdate>2007</risdate><spage>324</spage><epage>329</epage><pages>324-329</pages><issn>2150-6078</issn><isbn>9781424418718</isbn><isbn>1424418712</isbn><eisbn>9781424418725</eisbn><eisbn>1424418720</eisbn><abstract>The COMS (communication, ocean and meteorological satellite) EPS (electrical power subsystem) is derived from an enhanced Eurostar 3000. The COMS EPS can offer a bus power capability of 3 kW. The aim of this analysis is to verify the electrical compatibility of the interfaces which exist between COMS EPS equipments and external equipments. For each interface, this study checked the compatibility between equipments for the power links, commands, digital telemetry, analog telemetry and failure condition. In addition with this interface compatibility verification, this study outputs electrical and manufacturing constraints to be applied at harness level.</abstract><pub>IEEE</pub><doi>10.1109/ICPE.2007.4692402</doi><tpages>6</tpages></addata></record> |
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identifier | ISSN: 2150-6078 |
ispartof | 2007 7th Internatonal Conference on Power Electronics, 2007, p.324-329 |
issn | 2150-6078 |
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source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Aerospace electronics Batteries Frequency Fuses Manufacturing Performance analysis Power electronics Telemetry Voltage Wires |
title | Electrical interfaces compatibility analysis for the COMS EPS |
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