Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel
The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a ge...
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Veröffentlicht in: | Russian aeronautics 2020, Vol.63 (1), p.25-32 |
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container_title | Russian aeronautics |
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creator | Abdullina, E. Yu Efanov, V. N. |
description | The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a generalized characteristic of the system, which ensures the matching the states at an arbitrary moment of change of its operation mode. |
doi_str_mv | 10.3103/S1068799820010043 |
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Yu ; Efanov, V. N.</creator><creatorcontrib>Abdullina, E. Yu ; Efanov, V. N.</creatorcontrib><description>The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a generalized characteristic of the system, which ensures the matching the states at an arbitrary moment of change of its operation mode.</description><identifier>ISSN: 1068-7998</identifier><identifier>EISSN: 1934-7901</identifier><identifier>DOI: 10.3103/S1068799820010043</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Angle of attack ; Automotive Engineering ; Constraining ; Control systems ; Engineering ; Flight Dynamics and Control of Flight Vehicles ; Matching ; Pitch (inclination)</subject><ispartof>Russian aeronautics, 2020, Vol.63 (1), p.25-32</ispartof><rights>Allerton Press, Inc. 2020</rights><rights>Allerton Press, Inc. 2020.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c1833-96a4428df26524078438d9cc4020e3da4d289743f853bace7d65075495faacc83</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.3103/S1068799820010043$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.3103/S1068799820010043$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,780,784,27924,27925,41488,42557,51319</link.rule.ids></links><search><creatorcontrib>Abdullina, E. Yu</creatorcontrib><creatorcontrib>Efanov, V. N.</creatorcontrib><title>Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel</title><title>Russian aeronautics</title><addtitle>Russ. Aeronaut</addtitle><description>The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a generalized characteristic of the system, which ensures the matching the states at an arbitrary moment of change of its operation mode.</description><subject>Angle of attack</subject><subject>Automotive Engineering</subject><subject>Constraining</subject><subject>Control systems</subject><subject>Engineering</subject><subject>Flight Dynamics and Control of Flight Vehicles</subject><subject>Matching</subject><subject>Pitch (inclination)</subject><issn>1068-7998</issn><issn>1934-7901</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNp1kE9LAzEUxIMoWKsfwFvA8-rLn90kx7KoFSoK1fMSs9k2dZutSYr025tSxYN4egPzm3kwCF0SuGYE2M2cQCWFUpICEADOjtCIKMYLoYAcZ53tYu-forMYVwBlRTkdocf5zqeljS7iocPPLpklnvhFb3E9-BSGHs93Mdk1_nTpx8ngJCVt3vHMrV1yfoHrpfbe9ufopNN9tBffd4xe725f6mkxe7p_qCezwhDJWKEqzTmVbUerknIQkjPZKmM4ULCs1bylUgnOOlmyN22saKsSRMlV2WltjGRjdHXo3YThY2tjalbDNvj8ssl9jBBB-J4iB8qEIcZgu2YT3FqHXUOg2a_W_FktZ-ghEzPrFzb8Nv8f-gKgyWxe</recordid><startdate>2020</startdate><enddate>2020</enddate><creator>Abdullina, E. Yu</creator><creator>Efanov, V. N.</creator><general>Pleiades Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>2020</creationdate><title>Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel</title><author>Abdullina, E. Yu ; Efanov, V. N.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c1833-96a4428df26524078438d9cc4020e3da4d289743f853bace7d65075495faacc83</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Angle of attack</topic><topic>Automotive Engineering</topic><topic>Constraining</topic><topic>Control systems</topic><topic>Engineering</topic><topic>Flight Dynamics and Control of Flight Vehicles</topic><topic>Matching</topic><topic>Pitch (inclination)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Abdullina, E. Yu</creatorcontrib><creatorcontrib>Efanov, V. N.</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Russian aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Abdullina, E. Yu</au><au>Efanov, V. N.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel</atitle><jtitle>Russian aeronautics</jtitle><stitle>Russ. Aeronaut</stitle><date>2020</date><risdate>2020</risdate><volume>63</volume><issue>1</issue><spage>25</spage><epage>32</epage><pages>25-32</pages><issn>1068-7998</issn><eissn>1934-7901</eissn><abstract>The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a generalized characteristic of the system, which ensures the matching the states at an arbitrary moment of change of its operation mode.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.3103/S1068799820010043</doi><tpages>8</tpages></addata></record> |
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source | SpringerNature Journals |
subjects | Angle of attack Automotive Engineering Constraining Control systems Engineering Flight Dynamics and Control of Flight Vehicles Matching Pitch (inclination) |
title | Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel |
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