A novel analysis for tactical missile autopilot topologies
The available feedback topologies for tactical missile autopilot were detailed and examined using optimal control. There were transformations that could provide equivalent closed loop properties for the different topologies. The open loop properties of autopilots would be different, however. Compare...
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| creator | Fan Jun-Fang Sun Bao-Cai Su Zhong Dong Si-Yu |
| description | The available feedback topologies for tactical missile autopilot were detailed and examined using optimal control. There were transformations that could provide equivalent closed loop properties for the different topologies. The open loop properties of autopilots would be different, however. Compared with the limitations of traditional stability margins, a novel vector margin approach was introduced to establish a standard performance level and determine the best autopilot topology from a robustness perspective. A static unstable plant as example was used throughout. The analysis and simulation results validate the presented approach. |
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There were transformations that could provide equivalent closed loop properties for the different topologies. The open loop properties of autopilots would be different, however. Compared with the limitations of traditional stability margins, a novel vector margin approach was introduced to establish a standard performance level and determine the best autopilot topology from a robustness perspective. A static unstable plant as example was used throughout. The analysis and simulation results validate the presented approach.</description><identifier>ISSN: 1934-1768</identifier><identifier>ISBN: 1467325813</identifier><identifier>ISBN: 9781467325813</identifier><identifier>EISSN: 2161-2927</identifier><identifier>EISBN: 9789881563811</identifier><identifier>EISBN: 988156381X</identifier><language>eng</language><publisher>IEEE</publisher><subject>Acceleration ; Missile Autopilot ; Missiles ; Optimal control ; Robustness ; Stability analysis ; Topology ; Vector Margin ; Vectors</subject><ispartof>Proceedings of the 31st Chinese Control Conference, 2012, p.2316-2320</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/6390311$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2052,54895</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/6390311$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Fan Jun-Fang</creatorcontrib><creatorcontrib>Sun Bao-Cai</creatorcontrib><creatorcontrib>Su Zhong</creatorcontrib><creatorcontrib>Dong Si-Yu</creatorcontrib><title>A novel analysis for tactical missile autopilot topologies</title><title>Proceedings of the 31st Chinese Control Conference</title><addtitle>ChiCC</addtitle><description>The available feedback topologies for tactical missile autopilot were detailed and examined using optimal control. 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The analysis and simulation results validate the presented approach.</description><subject>Acceleration</subject><subject>Missile Autopilot</subject><subject>Missiles</subject><subject>Optimal control</subject><subject>Robustness</subject><subject>Stability analysis</subject><subject>Topology</subject><subject>Vector Margin</subject><subject>Vectors</subject><issn>1934-1768</issn><issn>2161-2927</issn><isbn>1467325813</isbn><isbn>9781467325813</isbn><isbn>9789881563811</isbn><isbn>988156381X</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2012</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotzMtKAzEUAND4Aqe1X-AmPzAwN3fyuO5KUSsU3Oi63MkkEkmbMhmF_r2Crs7uXIgVWUfOgTboAC5Fo8BAq0jZK7GA3lhU2gFeiwYI-xascbdiUetn15mOABvxsJbH8h2y5CPnc01VxjLJmf2cPGd5SLWmHCR_zeWUcpnlryWXjxTqnbiJnGtY_bsU70-Pb5ttu3t9ftmsd20Cq-fWGN8rizwwAitUg7WstY0qjhh47ElRRwwqUsRhBO2Ms95Z8DjSQBpxKe7_3hRC2J-mdODpvDdIHQLgD65BRgA</recordid><startdate>201207</startdate><enddate>201207</enddate><creator>Fan Jun-Fang</creator><creator>Sun Bao-Cai</creator><creator>Su Zhong</creator><creator>Dong Si-Yu</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>201207</creationdate><title>A novel analysis for tactical missile autopilot topologies</title><author>Fan Jun-Fang ; Sun Bao-Cai ; Su Zhong ; Dong Si-Yu</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i175t-66c4273aba31a232b77a557f2fd3ead492909a12f9f3bd158687c871c3d9b9533</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2012</creationdate><topic>Acceleration</topic><topic>Missile Autopilot</topic><topic>Missiles</topic><topic>Optimal control</topic><topic>Robustness</topic><topic>Stability analysis</topic><topic>Topology</topic><topic>Vector Margin</topic><topic>Vectors</topic><toplevel>online_resources</toplevel><creatorcontrib>Fan Jun-Fang</creatorcontrib><creatorcontrib>Sun Bao-Cai</creatorcontrib><creatorcontrib>Su Zhong</creatorcontrib><creatorcontrib>Dong Si-Yu</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 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>Fan Jun-Fang</au><au>Sun Bao-Cai</au><au>Su Zhong</au><au>Dong Si-Yu</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>A novel analysis for tactical missile autopilot topologies</atitle><btitle>Proceedings of the 31st Chinese Control Conference</btitle><stitle>ChiCC</stitle><date>2012-07</date><risdate>2012</risdate><spage>2316</spage><epage>2320</epage><pages>2316-2320</pages><issn>1934-1768</issn><eissn>2161-2927</eissn><isbn>1467325813</isbn><isbn>9781467325813</isbn><eisbn>9789881563811</eisbn><eisbn>988156381X</eisbn><abstract>The available feedback topologies for tactical missile autopilot were detailed and examined using optimal control. There were transformations that could provide equivalent closed loop properties for the different topologies. The open loop properties of autopilots would be different, however. Compared with the limitations of traditional stability margins, a novel vector margin approach was introduced to establish a standard performance level and determine the best autopilot topology from a robustness perspective. A static unstable plant as example was used throughout. The analysis and simulation results validate the presented approach.</abstract><pub>IEEE</pub><tpages>5</tpages></addata></record> |
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| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | Acceleration Missile Autopilot Missiles Optimal control Robustness Stability analysis Topology Vector Margin Vectors |
| title | A novel analysis for tactical missile autopilot topologies |
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