Problem of precision missile guidance: LQR and H super( infinity ) control frameworks
Addressed here is the precision missile guidance problem where the successful intercept criterion has been defined in terms of both minimizing the miss distance and controlling the missile body attitude with respect to the target at the terminal point. We show that the H super( infinity ) control th...
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| Veröffentlicht in: | IEEE transactions on aerospace and electronic systems 2003-01, Vol.39 (3) |
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| creator | Savkin, A V Pathirana, P N Faruqi, F A |
| description | Addressed here is the precision missile guidance problem where the successful intercept criterion has been defined in terms of both minimizing the miss distance and controlling the missile body attitude with respect to the target at the terminal point. We show that the H super( infinity ) control theory, when suitably modified, provides an effective framework for the precision missile guidance problem. The existence of feedback controllers (guidance laws) is investigated for the case of finite horizon and non-zero initial conditions. Both state feedback and output feedback implementations are explored. |
| doi_str_mv | 10.1109/TAES.2003.1238744 |
| format | Article |
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Both state feedback and output feedback implementations are explored.</description><subject>Control theory</subject><subject>Controllers</subject><subject>Criteria</subject><subject>Feedback</subject><subject>Initial conditions</subject><subject>Laws</subject><subject>Miss distance</subject><subject>Missiles</subject><issn>0018-9251</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2003</creationdate><recordtype>article</recordtype><recordid>eNqVjbsKwjAUQDMo-PwAtzvqYE2aaqubiOLg4HOWWG8lmiY1t0X8ex38AafDgQOHsZ7ggRB8OjrOl4cg5FwGIpRJHEU11uRcJMNpOBYN1iK6fzVKItlkp613F4M5uAwKj6km7SzkmkgbhFulr8qmOIPNbg_KXmENVBXo-6Btpq0u3zCA1NnSOwOZVzm-nH9Qh9UzZQi7P7ZZf7U8LtbDwrtnhVSev4cUjVEWXUVnMYmF5HEylvKP9ANuxkj9</recordid><startdate>20030101</startdate><enddate>20030101</enddate><creator>Savkin, A V</creator><creator>Pathirana, P N</creator><creator>Faruqi, F A</creator><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20030101</creationdate><title>Problem of precision missile guidance: LQR and H super( infinity ) control frameworks</title><author>Savkin, A V ; Pathirana, P N ; Faruqi, F A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-proquest_miscellaneous_16713078533</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2003</creationdate><topic>Control theory</topic><topic>Controllers</topic><topic>Criteria</topic><topic>Feedback</topic><topic>Initial conditions</topic><topic>Laws</topic><topic>Miss distance</topic><topic>Missiles</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Savkin, A V</creatorcontrib><creatorcontrib>Pathirana, P N</creatorcontrib><creatorcontrib>Faruqi, F A</creatorcontrib><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>IEEE transactions on aerospace and electronic systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Savkin, A V</au><au>Pathirana, P N</au><au>Faruqi, F A</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Problem of precision missile guidance: LQR and H super( infinity ) control frameworks</atitle><jtitle>IEEE transactions on aerospace and electronic systems</jtitle><date>2003-01-01</date><risdate>2003</risdate><volume>39</volume><issue>3</issue><issn>0018-9251</issn><abstract>Addressed here is the precision missile guidance problem where the successful intercept criterion has been defined in terms of both minimizing the miss distance and controlling the missile body attitude with respect to the target at the terminal point. 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| fulltext | fulltext |
| identifier | ISSN: 0018-9251 |
| ispartof | IEEE transactions on aerospace and electronic systems, 2003-01, Vol.39 (3) |
| issn | 0018-9251 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_1671307853 |
| source | IEEE Electronic Library (IEL) |
| subjects | Control theory Controllers Criteria Feedback Initial conditions Laws Miss distance Missiles |
| title | Problem of precision missile guidance: LQR and H super( infinity ) control frameworks |
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