A Simplified Dynamic Model of Space Shuttle Main Engine

This paper presents a simplified model of the space shuttle main engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at twenty five differenc operating points of the SSME. The simplified model was developed...

Full description

Saved in:
Bibliographic Details
Main Authors: Duyar, Ahmet, Eldem, Yasfi, Merrill, Walter, Guo, Ten-Huei
Format: Conference Proceeding
Language:English
Subjects:
Aerodynamics
Clocks
Control systems
Engines
Open loop systems
Predictive models
Space shuttles
Steady-state
Testing
Valves
Online Access:Request full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by
cites
container_end_page 2099
container_issue
container_start_page 2094
container_title
container_volume
creator Duyar, Ahmet
Eldem, Yasfi
Merrill, Walter
Guo, Ten-Huei
description This paper presents a simplified model of the space shuttle main engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at twenty five differenc operating points of the SSME. The simplified model was developed for use with a model-based diagnostic scheme for failure detection and diagnostics studies, as well as control design purposes.
doi_str_mv 10.23919/ACC.1991.4791767
format conference_proceeding
fullrecord <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_4791767</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>4791767</ieee_id><sourcerecordid>4791767</sourcerecordid><originalsourceid>FETCH-LOGICAL-i1317-2bf6496fa79f539f5cbf77f185e181e5a461ea78fc8493d8a67813c42f3f4cdf3</originalsourceid><addsrcrecordid>eNotj81Kw0AURgekUK19AHEzL5CYm_m5M8sQqxVaXETXZTq5V0eSNDR10be3YD84nN2BT4gHKPJSefBPVV3n4D3kGj2gxRtxVzj0ujTWlDMx90XmtDFqLpbT9FNcZgx65W8FVrJJ_dglTtTK5_MQ-hTl9tBSJw8smzFEks337-nUkdyGNMjV8JUGuhczDt1Ey6sX4vNl9VGvs83761tdbbIECjAr92y1txzQs1EX4p4RGZwhcEAmaAsU0HF02qvWBYsOVNQlK9axZbUQj__dRES78Zj6cDzvrjfVH9eyRNk</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>A Simplified Dynamic Model of Space Shuttle Main Engine</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Duyar, Ahmet ; Eldem, Yasfi ; Merrill, Walter ; Guo, Ten-Huei</creator><creatorcontrib>Duyar, Ahmet ; Eldem, Yasfi ; Merrill, Walter ; Guo, Ten-Huei</creatorcontrib><description>This paper presents a simplified model of the space shuttle main engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at twenty five differenc operating points of the SSME. The simplified model was developed for use with a model-based diagnostic scheme for failure detection and diagnostics studies, as well as control design purposes.</description><identifier>ISBN: 0879425652</identifier><identifier>ISBN: 9780879425654</identifier><identifier>DOI: 10.23919/ACC.1991.4791767</identifier><identifier>LCCN: 90-84553</identifier><language>eng</language><publisher>IEEE</publisher><subject>Aerodynamics ; Clocks ; Control systems ; Engines ; Open loop systems ; Predictive models ; Space shuttles ; Steady-state ; Testing ; Valves</subject><ispartof>1991 American Control Conference, 1991, p.2094-2099</ispartof><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/4791767$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,780,784,789,790,2058,27925,54920</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/4791767$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Duyar, Ahmet</creatorcontrib><creatorcontrib>Eldem, Yasfi</creatorcontrib><creatorcontrib>Merrill, Walter</creatorcontrib><creatorcontrib>Guo, Ten-Huei</creatorcontrib><title>A Simplified Dynamic Model of Space Shuttle Main Engine</title><title>1991 American Control Conference</title><addtitle>ACC</addtitle><description>This paper presents a simplified model of the space shuttle main engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at twenty five differenc operating points of the SSME. The simplified model was developed for use with a model-based diagnostic scheme for failure detection and diagnostics studies, as well as control design purposes.</description><subject>Aerodynamics</subject><subject>Clocks</subject><subject>Control systems</subject><subject>Engines</subject><subject>Open loop systems</subject><subject>Predictive models</subject><subject>Space shuttles</subject><subject>Steady-state</subject><subject>Testing</subject><subject>Valves</subject><isbn>0879425652</isbn><isbn>9780879425654</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>1991</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><recordid>eNotj81Kw0AURgekUK19AHEzL5CYm_m5M8sQqxVaXETXZTq5V0eSNDR10be3YD84nN2BT4gHKPJSefBPVV3n4D3kGj2gxRtxVzj0ujTWlDMx90XmtDFqLpbT9FNcZgx65W8FVrJJ_dglTtTK5_MQ-hTl9tBSJw8smzFEks337-nUkdyGNMjV8JUGuhczDt1Ey6sX4vNl9VGvs83761tdbbIECjAr92y1txzQs1EX4p4RGZwhcEAmaAsU0HF02qvWBYsOVNQlK9axZbUQj__dRES78Zj6cDzvrjfVH9eyRNk</recordid><startdate>199106</startdate><enddate>199106</enddate><creator>Duyar, Ahmet</creator><creator>Eldem, Yasfi</creator><creator>Merrill, Walter</creator><creator>Guo, Ten-Huei</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>199106</creationdate><title>A Simplified Dynamic Model of Space Shuttle Main Engine</title><author>Duyar, Ahmet ; Eldem, Yasfi ; Merrill, Walter ; Guo, Ten-Huei</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i1317-2bf6496fa79f539f5cbf77f185e181e5a461ea78fc8493d8a67813c42f3f4cdf3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>1991</creationdate><topic>Aerodynamics</topic><topic>Clocks</topic><topic>Control systems</topic><topic>Engines</topic><topic>Open loop systems</topic><topic>Predictive models</topic><topic>Space shuttles</topic><topic>Steady-state</topic><topic>Testing</topic><topic>Valves</topic><toplevel>online_resources</toplevel><creatorcontrib>Duyar, Ahmet</creatorcontrib><creatorcontrib>Eldem, Yasfi</creatorcontrib><creatorcontrib>Merrill, Walter</creatorcontrib><creatorcontrib>Guo, Ten-Huei</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/IET Electronic Library (IEL)</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>Duyar, Ahmet</au><au>Eldem, Yasfi</au><au>Merrill, Walter</au><au>Guo, Ten-Huei</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>A Simplified Dynamic Model of Space Shuttle Main Engine</atitle><btitle>1991 American Control Conference</btitle><stitle>ACC</stitle><date>1991-06</date><risdate>1991</risdate><spage>2094</spage><epage>2099</epage><pages>2094-2099</pages><isbn>0879425652</isbn><isbn>9780879425654</isbn><abstract>This paper presents a simplified model of the space shuttle main engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at twenty five differenc operating points of the SSME. The simplified model was developed for use with a model-based diagnostic scheme for failure detection and diagnostics studies, as well as control design purposes.</abstract><pub>IEEE</pub><doi>10.23919/ACC.1991.4791767</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier ISBN: 0879425652
ispartof 1991 American Control Conference, 1991, p.2094-2099
issn
language eng
recordid cdi_ieee_primary_4791767
source IEEE Electronic Library (IEL) Conference Proceedings
subjects Aerodynamics
Clocks
Control systems
Engines
Open loop systems
Predictive models
Space shuttles
Steady-state
Testing
Valves
title A Simplified Dynamic Model of Space Shuttle Main Engine
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-01T06%3A02%3A57IST&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=A%20Simplified%20Dynamic%20Model%20of%20Space%20Shuttle%20Main%20Engine&rft.btitle=1991%20American%20Control%20Conference&rft.au=Duyar,%20Ahmet&rft.date=1991-06&rft.spage=2094&rft.epage=2099&rft.pages=2094-2099&rft.isbn=0879425652&rft.isbn_list=9780879425654&rft_id=info:doi/10.23919/ACC.1991.4791767&rft_dat=%3Cieee_6IE%3E4791767%3C/ieee_6IE%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-i1317-2bf6496fa79f539f5cbf77f185e181e5a461ea78fc8493d8a67813c42f3f4cdf3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=4791767&rfr_iscdi=true