Missile Guidance Law Estimation Using Modified Interactive Multiple Model Filter
This paper presents an interactive multiple-model-based guidance law estimation filter. An antiship missile’s threat index, such as the remaining time of flight and impact angle, can be estimated by using the guidance law estimation filter. The filter bank of the filter was composed of models based...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2014-03, Vol.37 (2), p.484-496 |
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| container_title | Journal of guidance, control, and dynamics |
| container_volume | 37 |
| creator | Yun, Joongsup Ryoo, Chang-Kyung |
| description | This paper presents an interactive multiple-model-based guidance law estimation filter. An antiship missile’s threat index, such as the remaining time of flight and impact angle, can be estimated by using the guidance law estimation filter. The filter bank of the filter was composed of models based on proportional navigation and impact angle control guidance laws. In the guidance law estimation filter, state variables, rather than fixed values of navigation constant or impact angle, are used for estimation. To that end, the modified interactive multiple model, which is a modified version of the conventional interactive multiple model method is presented in this paper. The modified interactive multiple model method minimizes the degradation of estimation performance by systematic approach for different state vectors. The effectiveness of the modified interactive multiple model method and the performance of the guidance law estimation filter are examined through the numerical simulation of various engagement scenarios. |
| doi_str_mv | 10.2514/1.61327 |
| format | Article |
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An antiship missile’s threat index, such as the remaining time of flight and impact angle, can be estimated by using the guidance law estimation filter. The filter bank of the filter was composed of models based on proportional navigation and impact angle control guidance laws. In the guidance law estimation filter, state variables, rather than fixed values of navigation constant or impact angle, are used for estimation. To that end, the modified interactive multiple model, which is a modified version of the conventional interactive multiple model method is presented in this paper. The modified interactive multiple model method minimizes the degradation of estimation performance by systematic approach for different state vectors. The effectiveness of the modified interactive multiple model method and the performance of the guidance law estimation filter are examined through the numerical simulation of various engagement scenarios.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.61327</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Antiship missiles ; Conferences ; Filter banks ; Guidance (motion) ; Guidance systems ; Impact angle ; Interactive ; Kalman filters ; Law ; Mathematical analysis ; Mathematical models ; Missile control ; Missiles ; Navigation ; Probability ; Proportional navigation ; R&D ; Random variables ; Research & development ; Self defense ; State vectors ; Variables</subject><ispartof>Journal of guidance, control, and dynamics, 2014-03, Vol.37 (2), p.484-496</ispartof><rights>Copyright © 2013 by Joongsup Yun and Chang-Kyung Ryoo. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code and $10.00 in correspondence with the CCC.</rights><rights>Copyright © 2013 by Joongsup Yun and Chang-Kyung Ryoo. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code 1533-3884/14 and $10.00 in correspondence with the CCC.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a377t-50a76bfe54b4eba62295f74f7f55d65d24de9a14532aa5f40f39db81fe84334c3</citedby><cites>FETCH-LOGICAL-a377t-50a76bfe54b4eba62295f74f7f55d65d24de9a14532aa5f40f39db81fe84334c3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Yun, Joongsup</creatorcontrib><creatorcontrib>Ryoo, Chang-Kyung</creatorcontrib><title>Missile Guidance Law Estimation Using Modified Interactive Multiple Model Filter</title><title>Journal of guidance, control, and dynamics</title><description>This paper presents an interactive multiple-model-based guidance law estimation filter. An antiship missile’s threat index, such as the remaining time of flight and impact angle, can be estimated by using the guidance law estimation filter. The filter bank of the filter was composed of models based on proportional navigation and impact angle control guidance laws. In the guidance law estimation filter, state variables, rather than fixed values of navigation constant or impact angle, are used for estimation. To that end, the modified interactive multiple model, which is a modified version of the conventional interactive multiple model method is presented in this paper. The modified interactive multiple model method minimizes the degradation of estimation performance by systematic approach for different state vectors. The effectiveness of the modified interactive multiple model method and the performance of the guidance law estimation filter are examined through the numerical simulation of various engagement scenarios.</description><subject>Antiship missiles</subject><subject>Conferences</subject><subject>Filter banks</subject><subject>Guidance (motion)</subject><subject>Guidance systems</subject><subject>Impact angle</subject><subject>Interactive</subject><subject>Kalman filters</subject><subject>Law</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Missile control</subject><subject>Missiles</subject><subject>Navigation</subject><subject>Probability</subject><subject>Proportional navigation</subject><subject>R&D</subject><subject>Random variables</subject><subject>Research & development</subject><subject>Self defense</subject><subject>State vectors</subject><subject>Variables</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><recordid>eNp90F1LwzAUBuAgCs4p_oWCgnrRmc-mvZSxzcGGXrjrkDaJZGRtbVI__r3ReiEqXp2L9zmHwwvAKYITzBC9RpMMEcz3wAgxQlKS53QfjCAnKGWwgIfgyPsthIhkiI_A_dp6b51OFr1Vsq50spIvycwHu5PBNnWy8bZ-TNaNssZqlSzroDtZBfusk3Xvgm3jbky1S-bWxewYHBjpvD75mmOwmc8eprfp6m6xnN6sUkk4D_EVybPSaEZLqkuZYVwww6nhhjGVMYWp0oVElBEsJTMUGlKoMkdG55QQWpExuBzutl3z1GsfxM76Sjsna930XiCGYRFl5GNw9oNum76r43cC04Iynkf8n0IMwpzgPMuiuhhU1TXed9qItotVdW8CQfHRv0Dis_8ozwcprZTfbv1iV3-yIRatMsL0Ljb7Gsg7s-2O-g</recordid><startdate>20140301</startdate><enddate>20140301</enddate><creator>Yun, Joongsup</creator><creator>Ryoo, Chang-Kyung</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope></search><sort><creationdate>20140301</creationdate><title>Missile Guidance Law Estimation Using Modified Interactive Multiple Model Filter</title><author>Yun, Joongsup ; Ryoo, Chang-Kyung</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a377t-50a76bfe54b4eba62295f74f7f55d65d24de9a14532aa5f40f39db81fe84334c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2014</creationdate><topic>Antiship missiles</topic><topic>Conferences</topic><topic>Filter banks</topic><topic>Guidance (motion)</topic><topic>Guidance systems</topic><topic>Impact angle</topic><topic>Interactive</topic><topic>Kalman filters</topic><topic>Law</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Missile control</topic><topic>Missiles</topic><topic>Navigation</topic><topic>Probability</topic><topic>Proportional navigation</topic><topic>R&D</topic><topic>Random variables</topic><topic>Research & development</topic><topic>Self defense</topic><topic>State vectors</topic><topic>Variables</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Yun, Joongsup</creatorcontrib><creatorcontrib>Ryoo, Chang-Kyung</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace 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><jtitle>Journal of guidance, control, and dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Yun, Joongsup</au><au>Ryoo, Chang-Kyung</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Missile Guidance Law Estimation Using Modified Interactive Multiple Model Filter</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2014-03-01</date><risdate>2014</risdate><volume>37</volume><issue>2</issue><spage>484</spage><epage>496</epage><pages>484-496</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>This paper presents an interactive multiple-model-based guidance law estimation filter. An antiship missile’s threat index, such as the remaining time of flight and impact angle, can be estimated by using the guidance law estimation filter. The filter bank of the filter was composed of models based on proportional navigation and impact angle control guidance laws. In the guidance law estimation filter, state variables, rather than fixed values of navigation constant or impact angle, are used for estimation. To that end, the modified interactive multiple model, which is a modified version of the conventional interactive multiple model method is presented in this paper. The modified interactive multiple model method minimizes the degradation of estimation performance by systematic approach for different state vectors. 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| ispartof | Journal of guidance, control, and dynamics, 2014-03, Vol.37 (2), p.484-496 |
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| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Antiship missiles Conferences Filter banks Guidance (motion) Guidance systems Impact angle Interactive Kalman filters Law Mathematical analysis Mathematical models Missile control Missiles Navigation Probability Proportional navigation R&D Random variables Research & development Self defense State vectors Variables |
| title | Missile Guidance Law Estimation Using Modified Interactive Multiple Model Filter |
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