Active homing performance enhancement with multiple model radome slope estimation
Abstract In this paper, a new filter structure with the interacting multiple model (IMM) algorithm for estimating both the radome slope and target states is suggested to reduce the radome induced miss distance effectively in active homing engagements of a surface-to-air missile. The proposed filter...
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| Veröffentlicht in: | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2005-06, Vol.219 (3), p.217-224 |
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| container_title | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering |
| container_volume | 219 |
| creator | Song, T L Lee, D G Shin, S J |
| description | Abstract
In this paper, a new filter structure with the interacting multiple model (IMM) algorithm for estimating both the radome slope and target states is suggested to reduce the radome induced miss distance effectively in active homing engagements of a surface-to-air missile. The proposed filter in conjunction with proportional navigation guidance is tested by a series of simulation runs in three-dimensional engagement scenarios. Simulation results show that the proposed filter structure stabilizes the missile system and gives allowable miss distance in case of large incident lag that may cause system instability in the presence of the radome slope. |
| doi_str_mv | 10.1243/095441005X30234 |
| format | Article |
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In this paper, a new filter structure with the interacting multiple model (IMM) algorithm for estimating both the radome slope and target states is suggested to reduce the radome induced miss distance effectively in active homing engagements of a surface-to-air missile. The proposed filter in conjunction with proportional navigation guidance is tested by a series of simulation runs in three-dimensional engagement scenarios. Simulation results show that the proposed filter structure stabilizes the missile system and gives allowable miss distance in case of large incident lag that may cause system instability in the presence of the radome slope.</description><identifier>ISSN: 0954-4100</identifier><identifier>EISSN: 2041-3025</identifier><identifier>DOI: 10.1243/095441005X30234</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Aerodynamics ; Computer simulation ; Error analysis ; Missiles</subject><ispartof>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2005-06, Vol.219 (3), p.217-224</ispartof><rights>2005 Institution of Mechanical Engineers</rights><rights>Copyright Professional Engineering Publishing Ltd Jun 2005</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c398t-c415c4c35ffa9ea14f735fa86010749a8aaecc7f73692680878f048d274dddc93</citedby><cites>FETCH-LOGICAL-c398t-c415c4c35ffa9ea14f735fa86010749a8aaecc7f73692680878f048d274dddc93</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1243/095441005X30234$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1243/095441005X30234$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,780,784,21819,27924,27925,43621,43622</link.rule.ids></links><search><creatorcontrib>Song, T L</creatorcontrib><creatorcontrib>Lee, D G</creatorcontrib><creatorcontrib>Shin, S J</creatorcontrib><title>Active homing performance enhancement with multiple model radome slope estimation</title><title>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</title><description>Abstract
In this paper, a new filter structure with the interacting multiple model (IMM) algorithm for estimating both the radome slope and target states is suggested to reduce the radome induced miss distance effectively in active homing engagements of a surface-to-air missile. The proposed filter in conjunction with proportional navigation guidance is tested by a series of simulation runs in three-dimensional engagement scenarios. Simulation results show that the proposed filter structure stabilizes the missile system and gives allowable miss distance in case of large incident lag that may cause system instability in the presence of the radome slope.</description><subject>Aerodynamics</subject><subject>Computer simulation</subject><subject>Error analysis</subject><subject>Missiles</subject><issn>0954-4100</issn><issn>2041-3025</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2005</creationdate><recordtype>article</recordtype><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><sourceid>GNUQQ</sourceid><recordid>eNqNkU1LxDAQhoMouK6evQYPnqw7-WibHpfFL1gQQcFbCel0t0vT1KRV_PdmWUFYEHYuM5N53jckQ8glg1vGpZhBkUrJANJ3AVzIIzLhIFkSm_SYTLbTZDs-JWchbCBGmokJeZmboflEuna26Va0R187b3VnkGK33maL3UC_mmFN7dgOTd8ita7ClnpdOYs0tK6PcBgaq4fGdefkpNZtwIvfPCVv93evi8dk-fzwtJgvEyMKNSRGstRII9K61gVqJus81lplwCCXhVZaozF5PM0KnilQuapBqornsqoqU4gpud759t59jPH-0jbBYNvqDt0YSq5UDlLwQ8CMqfwQxxQymbEIXu2BGzf6Lr625EwwxZSECM12kPEuBI912fv4Rf67ZFBuN1bubSwqbnaKoFf4Z_kf_gPfbJTs</recordid><startdate>20050601</startdate><enddate>20050601</enddate><creator>Song, T L</creator><creator>Lee, D G</creator><creator>Shin, S J</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>3V.</scope><scope>7TB</scope><scope>7XB</scope><scope>88F</scope><scope>88I</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>F28</scope><scope>FR3</scope><scope>GNUQQ</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>KB.</scope><scope>L6V</scope><scope>L7M</scope><scope>M1Q</scope><scope>M2P</scope><scope>M7S</scope><scope>P5Z</scope><scope>P62</scope><scope>PDBOC</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope><scope>Q9U</scope><scope>7SC</scope><scope>7SP</scope><scope>JQ2</scope><scope>L~C</scope><scope>L~D</scope></search><sort><creationdate>20050601</creationdate><title>Active homing performance enhancement with multiple model radome slope estimation</title><author>Song, T L ; 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Part G, Journal of aerospace engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Song, T L</au><au>Lee, D G</au><au>Shin, S J</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Active homing performance enhancement with multiple model radome slope estimation</atitle><jtitle>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</jtitle><date>2005-06-01</date><risdate>2005</risdate><volume>219</volume><issue>3</issue><spage>217</spage><epage>224</epage><pages>217-224</pages><issn>0954-4100</issn><eissn>2041-3025</eissn><abstract>Abstract
In this paper, a new filter structure with the interacting multiple model (IMM) algorithm for estimating both the radome slope and target states is suggested to reduce the radome induced miss distance effectively in active homing engagements of a surface-to-air missile. The proposed filter in conjunction with proportional navigation guidance is tested by a series of simulation runs in three-dimensional engagement scenarios. Simulation results show that the proposed filter structure stabilizes the missile system and gives allowable miss distance in case of large incident lag that may cause system instability in the presence of the radome slope.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1243/095441005X30234</doi><tpages>8</tpages></addata></record> |
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| ispartof | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2005-06, Vol.219 (3), p.217-224 |
| issn | 0954-4100 2041-3025 |
| language | eng |
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| source | Access via SAGE |
| subjects | Aerodynamics Computer simulation Error analysis Missiles |
| title | Active homing performance enhancement with multiple model radome slope estimation |
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