An Elementary Proof Of the Optimality of Hohmann Transfers
The Hohmann (1925) transfer is analytically proved by means of a gradient method to be the optimal two-impulse transfer between coplanar circular orbits in a central force field with a Newtonian attraction. By an extension of the method, it is further shown that a Hohmann-type transfer is the optima...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 1984-09, Vol.7 (5), p.629-630 |
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creator | Palmore, Julian |
description | The Hohmann (1925) transfer is analytically proved by means of a gradient method to be the optimal two-impulse transfer between coplanar circular orbits in a central force field with a Newtonian attraction. By an extension of the method, it is further shown that a Hohmann-type transfer is the optimal two-impulse transfer between coplanar orbits, one of which is circular and the other elliptical. The gradient method clearly shows that the characteristic velocity attains a minimum on the boundary of the region where the transfer orbits lie. |
doi_str_mv | 10.2514/3.56375 |
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By an extension of the method, it is further shown that a Hohmann-type transfer is the optimal two-impulse transfer between coplanar orbits, one of which is circular and the other elliptical. The gradient method clearly shows that the characteristic velocity attains a minimum on the boundary of the region where the transfer orbits lie.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/3.56375</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Aircraft ; Feedback ; Orbits ; Velocity</subject><ispartof>Journal of guidance, control, and dynamics, 1984-09, Vol.7 (5), p.629-630</ispartof><rights>Copyright American Institute of Aeronautics and Astronautics Sep/Oct 1984</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a345t-2d67aa269ba16c532a2d845ee2ed22e3660d282ce4603824ee86dc7fb02fcb383</citedby><cites>FETCH-LOGICAL-a345t-2d67aa269ba16c532a2d845ee2ed22e3660d282ce4603824ee86dc7fb02fcb383</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>Palmore, Julian</creatorcontrib><title>An Elementary Proof Of the Optimality of Hohmann Transfers</title><title>Journal of guidance, control, and dynamics</title><description>The Hohmann (1925) transfer is analytically proved by means of a gradient method to be the optimal two-impulse transfer between coplanar circular orbits in a central force field with a Newtonian attraction. By an extension of the method, it is further shown that a Hohmann-type transfer is the optimal two-impulse transfer between coplanar orbits, one of which is circular and the other elliptical. The gradient method clearly shows that the characteristic velocity attains a minimum on the boundary of the region where the transfer orbits lie.</description><subject>Aircraft</subject><subject>Feedback</subject><subject>Orbits</subject><subject>Velocity</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1984</creationdate><recordtype>article</recordtype><recordid>eNpt0E1Lw0AQBuBFFKxV_AsBRfGQujuTbDbeSqkfUKiHel62ySxNyZe7Cdh_b7QFQT0NzDwMMy9jl4JPIBbRPU5iiUl8xEYiRgxRqeiYjXiCIox5yk_ZmfdbzgVKkYzYw7QO5iVVVHfG7YJX1zQ2WNqg21CwbLuiMmXR7YKh-dxsKlPXwcqZ2lty_pydWFN6ujjUMXt7nK9mz-Fi-fQymy5Cg1HchZDLxBiQ6doImcUIBnIVxURAOQChlDwHBRlFkqOCiEjJPEvsmoPN1qhwzG72e1vXvPfkO10VPqOyNDU1vdcQQZpyAQO8-gW3Te_q4TYNKFBxUAkf1O1eZa7x3pHVrRvedDstuP5KUKP-TnCQ13tpCmN-dv1ld_-xw1i3udW2L8uOPjr8BA2fem0</recordid><startdate>19840901</startdate><enddate>19840901</enddate><creator>Palmore, Julian</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>19840901</creationdate><title>An Elementary Proof Of the Optimality of Hohmann Transfers</title><author>Palmore, Julian</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a345t-2d67aa269ba16c532a2d845ee2ed22e3660d282ce4603824ee86dc7fb02fcb383</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1984</creationdate><topic>Aircraft</topic><topic>Feedback</topic><topic>Orbits</topic><topic>Velocity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Palmore, Julian</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>Palmore, Julian</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>An Elementary Proof Of the Optimality of Hohmann Transfers</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>1984-09-01</date><risdate>1984</risdate><volume>7</volume><issue>5</issue><spage>629</spage><epage>630</epage><pages>629-630</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>The Hohmann (1925) transfer is analytically proved by means of a gradient method to be the optimal two-impulse transfer between coplanar circular orbits in a central force field with a Newtonian attraction. By an extension of the method, it is further shown that a Hohmann-type transfer is the optimal two-impulse transfer between coplanar orbits, one of which is circular and the other elliptical. The gradient method clearly shows that the characteristic velocity attains a minimum on the boundary of the region where the transfer orbits lie.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.56375</doi><tpages>2</tpages></addata></record> |
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subjects | Aircraft Feedback Orbits Velocity |
title | An Elementary Proof Of the Optimality of Hohmann Transfers |
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