Modeling nonlinear loads for aerospace power systems

More and more electronic equipment is being added to airplane electrical systems. The addition of these nonlinear loads could result in a number of power quality problems when the system is fully integrated. These disturbances include excessive harmonic distortion, voltage sags, transient voltages o...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Karimi, K.J., Mong, A.C.
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 38
container_issue
container_start_page 33
container_title
container_volume
creator Karimi, K.J.
Mong, A.C.
description More and more electronic equipment is being added to airplane electrical systems. The addition of these nonlinear loads could result in a number of power quality problems when the system is fully integrated. These disturbances include excessive harmonic distortion, voltage sags, transient voltages outside specified limits, and power transfer problems. We will describe modeling and simulation of nonlinear loads for aerospace power systems using Saber simulation software. These modeling tools help in developing and validating requirements, predicting power quality disturbances before the power system is fully integrated, troubleshooting once the system is fully integrated, and verification of the system. We will describe modeling a suite of nonlinear single phase and three-phase loads including various types of rectifiers including 6-pulse, 12-pulse, and 18-pulse circuits. We will also present system simulation studies using these nonlinear models and various types of linear models. System studies include the use of corrective measures such as the use active power factor correction (PFC) circuits that are used to reduce harmonic distortion.
doi_str_mv 10.1109/IECEC.2002.1391970
format Conference Proceeding
fullrecord <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_1391970</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>1391970</ieee_id><sourcerecordid>1391970</sourcerecordid><originalsourceid>FETCH-ieee_primary_13919703</originalsourceid><addsrcrecordid>eNp9jrsOgjAUQG9iTHzxA7r0B8RbqNTOBKODGztp5GIw0JJeE8Pfy8DsWc5wlgOwlxhLieZ0L_IijxPEJJapkUbjAjaoL5jqxGRqBRHzGyfUWeosW4N6-Jq61r2E824y2SA6b2sWjQ_CUvA82CeJwX8pCB75Qz3vYNnYjimavYXDtSjz27ElomoIbW_DWM0D6f_6AyBMNPU</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Modeling nonlinear loads for aerospace power systems</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Karimi, K.J. ; Mong, A.C.</creator><creatorcontrib>Karimi, K.J. ; Mong, A.C.</creatorcontrib><description>More and more electronic equipment is being added to airplane electrical systems. The addition of these nonlinear loads could result in a number of power quality problems when the system is fully integrated. These disturbances include excessive harmonic distortion, voltage sags, transient voltages outside specified limits, and power transfer problems. We will describe modeling and simulation of nonlinear loads for aerospace power systems using Saber simulation software. These modeling tools help in developing and validating requirements, predicting power quality disturbances before the power system is fully integrated, troubleshooting once the system is fully integrated, and verification of the system. We will describe modeling a suite of nonlinear single phase and three-phase loads including various types of rectifiers including 6-pulse, 12-pulse, and 18-pulse circuits. We will also present system simulation studies using these nonlinear models and various types of linear models. System studies include the use of corrective measures such as the use active power factor correction (PFC) circuits that are used to reduce harmonic distortion.</description><identifier>ISBN: 0780372964</identifier><identifier>ISBN: 9780780372962</identifier><identifier>DOI: 10.1109/IECEC.2002.1391970</identifier><language>eng</language><publisher>IEEE</publisher><subject>Aerospace simulation ; Circuits ; Electronic equipment ; Harmonic distortion ; Load modeling ; Power quality ; Power system harmonics ; Power system modeling ; Power system simulation ; Power system transients</subject><ispartof>IECEC '02. 2002 37th Intersociety Energy Conversion Engineering Conference, 2002, 2002, p.33-38</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/1391970$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,780,784,789,790,2058,4050,4051,27925,54920</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/1391970$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Karimi, K.J.</creatorcontrib><creatorcontrib>Mong, A.C.</creatorcontrib><title>Modeling nonlinear loads for aerospace power systems</title><title>IECEC '02. 2002 37th Intersociety Energy Conversion Engineering Conference, 2002</title><addtitle>IECEC</addtitle><description>More and more electronic equipment is being added to airplane electrical systems. The addition of these nonlinear loads could result in a number of power quality problems when the system is fully integrated. These disturbances include excessive harmonic distortion, voltage sags, transient voltages outside specified limits, and power transfer problems. We will describe modeling and simulation of nonlinear loads for aerospace power systems using Saber simulation software. These modeling tools help in developing and validating requirements, predicting power quality disturbances before the power system is fully integrated, troubleshooting once the system is fully integrated, and verification of the system. We will describe modeling a suite of nonlinear single phase and three-phase loads including various types of rectifiers including 6-pulse, 12-pulse, and 18-pulse circuits. We will also present system simulation studies using these nonlinear models and various types of linear models. System studies include the use of corrective measures such as the use active power factor correction (PFC) circuits that are used to reduce harmonic distortion.</description><subject>Aerospace simulation</subject><subject>Circuits</subject><subject>Electronic equipment</subject><subject>Harmonic distortion</subject><subject>Load modeling</subject><subject>Power quality</subject><subject>Power system harmonics</subject><subject>Power system modeling</subject><subject>Power system simulation</subject><subject>Power system transients</subject><isbn>0780372964</isbn><isbn>9780780372962</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2002</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNp9jrsOgjAUQG9iTHzxA7r0B8RbqNTOBKODGztp5GIw0JJeE8Pfy8DsWc5wlgOwlxhLieZ0L_IijxPEJJapkUbjAjaoL5jqxGRqBRHzGyfUWeosW4N6-Jq61r2E824y2SA6b2sWjQ_CUvA82CeJwX8pCB75Qz3vYNnYjimavYXDtSjz27ElomoIbW_DWM0D6f_6AyBMNPU</recordid><startdate>2002</startdate><enddate>2002</enddate><creator>Karimi, K.J.</creator><creator>Mong, A.C.</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>2002</creationdate><title>Modeling nonlinear loads for aerospace power systems</title><author>Karimi, K.J. ; Mong, A.C.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-ieee_primary_13919703</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2002</creationdate><topic>Aerospace simulation</topic><topic>Circuits</topic><topic>Electronic equipment</topic><topic>Harmonic distortion</topic><topic>Load modeling</topic><topic>Power quality</topic><topic>Power system harmonics</topic><topic>Power system modeling</topic><topic>Power system simulation</topic><topic>Power system transients</topic><toplevel>online_resources</toplevel><creatorcontrib>Karimi, K.J.</creatorcontrib><creatorcontrib>Mong, A.C.</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>Karimi, K.J.</au><au>Mong, A.C.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Modeling nonlinear loads for aerospace power systems</atitle><btitle>IECEC '02. 2002 37th Intersociety Energy Conversion Engineering Conference, 2002</btitle><stitle>IECEC</stitle><date>2002</date><risdate>2002</risdate><spage>33</spage><epage>38</epage><pages>33-38</pages><isbn>0780372964</isbn><isbn>9780780372962</isbn><abstract>More and more electronic equipment is being added to airplane electrical systems. The addition of these nonlinear loads could result in a number of power quality problems when the system is fully integrated. These disturbances include excessive harmonic distortion, voltage sags, transient voltages outside specified limits, and power transfer problems. We will describe modeling and simulation of nonlinear loads for aerospace power systems using Saber simulation software. These modeling tools help in developing and validating requirements, predicting power quality disturbances before the power system is fully integrated, troubleshooting once the system is fully integrated, and verification of the system. We will describe modeling a suite of nonlinear single phase and three-phase loads including various types of rectifiers including 6-pulse, 12-pulse, and 18-pulse circuits. We will also present system simulation studies using these nonlinear models and various types of linear models. System studies include the use of corrective measures such as the use active power factor correction (PFC) circuits that are used to reduce harmonic distortion.</abstract><pub>IEEE</pub><doi>10.1109/IECEC.2002.1391970</doi></addata></record>
fulltext fulltext_linktorsrc
identifier ISBN: 0780372964
ispartof IECEC '02. 2002 37th Intersociety Energy Conversion Engineering Conference, 2002, 2002, p.33-38
issn
language eng
recordid cdi_ieee_primary_1391970
source IEEE Electronic Library (IEL) Conference Proceedings
subjects Aerospace simulation
Circuits
Electronic equipment
Harmonic distortion
Load modeling
Power quality
Power system harmonics
Power system modeling
Power system simulation
Power system transients
title Modeling nonlinear loads for aerospace power systems
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-03T18%3A59%3A06IST&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=Modeling%20nonlinear%20loads%20for%20aerospace%20power%20systems&rft.btitle=IECEC%20'02.%202002%2037th%20Intersociety%20Energy%20Conversion%20Engineering%20Conference,%202002&rft.au=Karimi,%20K.J.&rft.date=2002&rft.spage=33&rft.epage=38&rft.pages=33-38&rft.isbn=0780372964&rft.isbn_list=9780780372962&rft_id=info:doi/10.1109/IECEC.2002.1391970&rft_dat=%3Cieee_6IE%3E1391970%3C/ieee_6IE%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=1391970&rfr_iscdi=true