Simulation and control of a 20-kHz spacecraft power system
A detailed computer representation of four Mapham inverters connected in a series-parallel arrangement has been implemented. System performance is illustrated by computer traces for the four Mapham inverters connected to a Litz cable with parallel resistance and DC receiver loads at the receiving en...
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Veröffentlicht in: | IEEE transactions on aerospace and electronic systems 1989-09, Vol.25 (5), p.668-676 |
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creator | Wasynczuk, O. Krause, P.C. |
description | A detailed computer representation of four Mapham inverters connected in a series-parallel arrangement has been implemented. System performance is illustrated by computer traces for the four Mapham inverters connected to a Litz cable with parallel resistance and DC receiver loads at the receiving end of the transmission cable. Methods of voltage control and load sharing between the inverters are demonstrated. The computer representation is used to design and demonstrate the advantages of a feedforward voltage-control strategy. It is shown that with a computer simulation of this type, the performance and control of spacecraft power systems can be investigated with relative ease and facility.< > |
doi_str_mv | 10.1109/7.42084 |
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System performance is illustrated by computer traces for the four Mapham inverters connected to a Litz cable with parallel resistance and DC receiver loads at the receiving end of the transmission cable. Methods of voltage control and load sharing between the inverters are demonstrated. The computer representation is used to design and demonstrate the advantages of a feedforward voltage-control strategy. It is shown that with a computer simulation of this type, the performance and control of spacecraft power systems can be investigated with relative ease and facility.< ></description><identifier>ISSN: 0018-9251</identifier><identifier>EISSN: 1557-9603</identifier><identifier>DOI: 10.1109/7.42084</identifier><identifier>CODEN: IEARAX</identifier><language>eng</language><publisher>New York, NY: IEEE</publisher><subject>Applied sciences ; Computational modeling ; Concurrent computing ; Electrical engineering. 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System performance is illustrated by computer traces for the four Mapham inverters connected to a Litz cable with parallel resistance and DC receiver loads at the receiving end of the transmission cable. Methods of voltage control and load sharing between the inverters are demonstrated. The computer representation is used to design and demonstrate the advantages of a feedforward voltage-control strategy. It is shown that with a computer simulation of this type, the performance and control of spacecraft power systems can be investigated with relative ease and facility.< ></description><subject>Applied sciences</subject><subject>Computational modeling</subject><subject>Concurrent computing</subject><subject>Electrical engineering. Electrical power engineering</subject><subject>Exact sciences and technology</subject><subject>Inverters</subject><subject>Power cables</subject><subject>Power electronics, power supplies</subject><subject>Power system control</subject><subject>Power system simulation</subject><subject>Power systems</subject><subject>Space vehicles</subject><subject>System performance</subject><subject>Voltage control</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1989</creationdate><recordtype>article</recordtype><recordid>eNqN0M9LwzAUB_AgCs4pnr3lop4687uJNxnqhIEH9Ryy9BWqbVOTDtn-eqsdetTT4_E-fOF9ETqlZEYpMVf5TDCixR6aUCnzzCjC99GEEKozwyQ9REcpvQ6r0IJP0PVT1axr11ehxa4tsA9tH0ONQ4kdZiR7W2xx6pwHH13Z4y58QMRpk3pojtFB6eoEJ7s5RS93t8_zRbZ8vH-Y3ywzz5Xos1yQQimgyjAmueMFp2CY4k56Z3JdFrygOmerlfKCCAqaiUJLxhU10oOkfIouxtwuhvc1pN42VfJQ166FsE6WGcKN0P-AWnEpNfkbSiEVUWqAlyP0MaQUobRdrBoXN5YS-9W2ze1324M830W65F1dRtf6Kv3y4VOWCz24s9FVAPBzHjM-ATQHgzY</recordid><startdate>19890901</startdate><enddate>19890901</enddate><creator>Wasynczuk, O.</creator><creator>Krause, P.C.</creator><general>IEEE</general><general>Institute of Electrical and Electronics Engineers</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>8FD</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>7TB</scope><scope>FR3</scope><scope>H8D</scope></search><sort><creationdate>19890901</creationdate><title>Simulation and control of a 20-kHz spacecraft power system</title><author>Wasynczuk, O. ; Krause, P.C.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c364t-740d66e1692253a3d31e9263a5ca978fd3d1872bb6c4041e824d85236195ce513</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1989</creationdate><topic>Applied sciences</topic><topic>Computational modeling</topic><topic>Concurrent computing</topic><topic>Electrical engineering. Electrical power engineering</topic><topic>Exact sciences and technology</topic><topic>Inverters</topic><topic>Power cables</topic><topic>Power electronics, power supplies</topic><topic>Power system control</topic><topic>Power system simulation</topic><topic>Power systems</topic><topic>Space vehicles</topic><topic>System performance</topic><topic>Voltage control</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wasynczuk, O.</creatorcontrib><creatorcontrib>Krause, P.C.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><jtitle>IEEE transactions on aerospace and electronic systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Wasynczuk, O.</au><au>Krause, P.C.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Simulation and control of a 20-kHz spacecraft power system</atitle><jtitle>IEEE transactions on aerospace and electronic systems</jtitle><stitle>T-AES</stitle><date>1989-09-01</date><risdate>1989</risdate><volume>25</volume><issue>5</issue><spage>668</spage><epage>676</epage><pages>668-676</pages><issn>0018-9251</issn><eissn>1557-9603</eissn><coden>IEARAX</coden><abstract>A detailed computer representation of four Mapham inverters connected in a series-parallel arrangement has been implemented. System performance is illustrated by computer traces for the four Mapham inverters connected to a Litz cable with parallel resistance and DC receiver loads at the receiving end of the transmission cable. Methods of voltage control and load sharing between the inverters are demonstrated. The computer representation is used to design and demonstrate the advantages of a feedforward voltage-control strategy. It is shown that with a computer simulation of this type, the performance and control of spacecraft power systems can be investigated with relative ease and facility.< ></abstract><cop>New York, NY</cop><pub>IEEE</pub><doi>10.1109/7.42084</doi><tpages>9</tpages></addata></record> |
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source | IEEE Electronic Library (IEL) |
subjects | Applied sciences Computational modeling Concurrent computing Electrical engineering. Electrical power engineering Exact sciences and technology Inverters Power cables Power electronics, power supplies Power system control Power system simulation Power systems Space vehicles System performance Voltage control |
title | Simulation and control of a 20-kHz spacecraft power system |
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