Onboard near-optimal climb-dash energy management
This paper studies optimal and near-optimal trajectories of high-performance aircraft in symmetric flight. Onboard, real-time, near-optimal guidance is considered for the climb-dash mission, using some of the boundary-layer structure and hierarchical ideas from singular perturbations. In the case of...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 1985-05, Vol.8 (3), p.320-324 |
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container_title | Journal of guidance, control, and dynamics |
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creator | WESTON, A CLIFF, G KELLEY, H |
description | This paper studies optimal and near-optimal trajectories of high-performance aircraft in symmetric flight. Onboard, real-time, near-optimal guidance is considered for the climb-dash mission, using some of the boundary-layer structure and hierarchical ideas from singular perturbations. In the case of symmetric flight, this resembles neighborhood-optimal guidance using energy-to-go as the running variable. However, extension to three-dimensional flight is proposed, using families of nominal paths with heading-to-go as the additional running variable. Some computational results are presented for the symmetric case. |
doi_str_mv | 10.2514/3.19982 |
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Onboard, real-time, near-optimal guidance is considered for the climb-dash mission, using some of the boundary-layer structure and hierarchical ideas from singular perturbations. In the case of symmetric flight, this resembles neighborhood-optimal guidance using energy-to-go as the running variable. However, extension to three-dimensional flight is proposed, using families of nominal paths with heading-to-go as the additional running variable. Some computational results are presented for the symmetric case.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/3.19982</identifier><language>eng</language><publisher>Legacy CDMS: American Institute of Aeronautics and Astronautics</publisher><subject>Aerospace engineering ; Aircraft ; Aircraft Design, Testing And Performance ; aircraft engineering ; Algorithms ; Altitude ; Energy management ; Energy modeling ; flight control systems ; guidance and control systems ; optimal control</subject><ispartof>Journal of guidance, control, and dynamics, 1985-05, Vol.8 (3), p.320-324</ispartof><rights>Copyright American Institute of Aeronautics and Astronautics May/Jun 1985</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a460t-5debdad054803df67820dce79719e3dfbdb30c2a022eeb20d83acb301602ca283</citedby><cites>FETCH-LOGICAL-a460t-5debdad054803df67820dce79719e3dfbdb30c2a022eeb20d83acb301602ca283</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>WESTON, A</creatorcontrib><creatorcontrib>CLIFF, G</creatorcontrib><creatorcontrib>KELLEY, H</creatorcontrib><title>Onboard near-optimal climb-dash energy management</title><title>Journal of guidance, control, and dynamics</title><description>This paper studies optimal and near-optimal trajectories of high-performance aircraft in symmetric flight. 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Some computational results are presented for the symmetric case.</description><subject>Aerospace engineering</subject><subject>Aircraft</subject><subject>Aircraft Design, Testing And Performance</subject><subject>aircraft engineering</subject><subject>Algorithms</subject><subject>Altitude</subject><subject>Energy management</subject><subject>Energy modeling</subject><subject>flight control systems</subject><subject>guidance and control systems</subject><subject>optimal control</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1985</creationdate><recordtype>article</recordtype><sourceid>CYI</sourceid><recordid>eNqNkUtLxDAQx4MouD7wC3hYUBQP1UnSPHoU8QULe9FzmDaprrRpTVpwv71ZVxBEZE8D8__N6z-EHFG4ZILmV_ySFoVmW2RCBecZ1zrfJhNQnGYCCtglezG-AVAuqZoQOvdlh8FOvcOQdf2waLGZVs2iLTOL8XXqvAsvy2mLHl9c6_xwQHZqbKI7_I775Pnu9unmIZvN7x9vrmcZ5hKGTFhXWrQgcg3c1lJpBrZyqlC0cClR2pJDxRAYc65MmuZYpRSVwCpkmu-T83XfPnTvo4uDaRexck2D3nVjNCoXUiop8kSe_UuyXAqldbEZKAu6ESglXy158gt868bgky-Gcco1FUIVP6dUoYsxuNr0IfkcloaCWT3NcPP1tEQer0mPEY0fQkyCFgACJIckX6xlXCD-jPquNr2tTT02zeA-hsSe_sX-nvgJeE6o1w</recordid><startdate>19850501</startdate><enddate>19850501</enddate><creator>WESTON, A</creator><creator>CLIFF, G</creator><creator>KELLEY, H</creator><general>American Institute of Aeronautics and Astronautics</general><scope>CYE</scope><scope>CYI</scope><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><scope>7TC</scope></search><sort><creationdate>19850501</creationdate><title>Onboard near-optimal climb-dash energy management</title><author>WESTON, A ; CLIFF, G ; KELLEY, H</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a460t-5debdad054803df67820dce79719e3dfbdb30c2a022eeb20d83acb301602ca283</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1985</creationdate><topic>Aerospace engineering</topic><topic>Aircraft</topic><topic>Aircraft Design, Testing And Performance</topic><topic>aircraft engineering</topic><topic>Algorithms</topic><topic>Altitude</topic><topic>Energy management</topic><topic>Energy modeling</topic><topic>flight control systems</topic><topic>guidance and control systems</topic><topic>optimal control</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>WESTON, A</creatorcontrib><creatorcontrib>CLIFF, G</creatorcontrib><creatorcontrib>KELLEY, H</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection><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><collection>Mechanical Engineering Abstracts</collection><jtitle>Journal of guidance, control, and dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>WESTON, A</au><au>CLIFF, G</au><au>KELLEY, H</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Onboard near-optimal climb-dash energy management</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>1985-05-01</date><risdate>1985</risdate><volume>8</volume><issue>3</issue><spage>320</spage><epage>324</epage><pages>320-324</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>This paper studies optimal and near-optimal trajectories of high-performance aircraft in symmetric flight. Onboard, real-time, near-optimal guidance is considered for the climb-dash mission, using some of the boundary-layer structure and hierarchical ideas from singular perturbations. In the case of symmetric flight, this resembles neighborhood-optimal guidance using energy-to-go as the running variable. However, extension to three-dimensional flight is proposed, using families of nominal paths with heading-to-go as the additional running variable. Some computational results are presented for the symmetric case.</abstract><cop>Legacy CDMS</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.19982</doi><tpages>5</tpages></addata></record> |
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source | NASA Technical Reports Server; Alma/SFX Local Collection |
subjects | Aerospace engineering Aircraft Aircraft Design, Testing And Performance aircraft engineering Algorithms Altitude Energy management Energy modeling flight control systems guidance and control systems optimal control |
title | Onboard near-optimal climb-dash energy management |
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