A qualitative study of proportional navigation
This paper represents a study of the trajectories of an ideal missile homing on a target according to the proportional navigation law. A qualitative study is performed and conditions are determined which enable one to demonstrate that: 1) the missile always reaches the target regardless of the initi...
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| Veröffentlicht in: | IEEE transactions on aerospace and electronic systems 1971-07, Vol.AES-7 (4), p.637-643 |
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| container_title | IEEE transactions on aerospace and electronic systems |
| container_volume | AES-7 |
| creator | Guelman, Mauricio |
| description | This paper represents a study of the trajectories of an ideal missile homing on a target according to the proportional navigation law. A qualitative study is performed and conditions are determined which enable one to demonstrate that: 1) the missile always reaches the target regardless of the initial conditions at launch; 2) the rotational rate of the line of sight is decreasing at the pursuit end. |
| doi_str_mv | 10.1109/TAES.1971.310406 |
| format | Article |
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A qualitative study is performed and conditions are determined which enable one to demonstrate that: 1) the missile always reaches the target regardless of the initial conditions at launch; 2) the rotational rate of the line of sight is decreasing at the pursuit end.</description><identifier>ISSN: 0018-9251</identifier><identifier>EISSN: 1557-9603</identifier><identifier>DOI: 10.1109/TAES.1971.310406</identifier><identifier>CODEN: IEARAX</identifier><language>eng</language><publisher>IEEE</publisher><subject>Aerodynamics ; Differential equations ; Geometry ; Kinematics ; Missiles ; Navigation ; Proportional control ; Time varying systems ; Trajectory</subject><ispartof>IEEE transactions on aerospace and electronic systems, 1971-07, Vol.AES-7 (4), p.637-643</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c261t-660216dad211d0b7a1f01363563d5af49ec15ed091f21496767ab9b49ce1da4d3</citedby><cites>FETCH-LOGICAL-c261t-660216dad211d0b7a1f01363563d5af49ec15ed091f21496767ab9b49ce1da4d3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/4103772$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,776,780,792,27903,27904,54737</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/4103772$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Guelman, Mauricio</creatorcontrib><title>A qualitative study of proportional navigation</title><title>IEEE transactions on aerospace and electronic systems</title><addtitle>T-AES</addtitle><description>This paper represents a study of the trajectories of an ideal missile homing on a target according to the proportional navigation law. A qualitative study is performed and conditions are determined which enable one to demonstrate that: 1) the missile always reaches the target regardless of the initial conditions at launch; 2) the rotational rate of the line of sight is decreasing at the pursuit end.</description><subject>Aerodynamics</subject><subject>Differential equations</subject><subject>Geometry</subject><subject>Kinematics</subject><subject>Missiles</subject><subject>Navigation</subject><subject>Proportional control</subject><subject>Time varying systems</subject><subject>Trajectory</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1971</creationdate><recordtype>article</recordtype><recordid>eNo9j11LwzAYhYMoOKf3gjf9A63vm8_lsoz5AQMvnNchbRKJ1LUm3WD_3pWKV4cD5znwEHKPUCGCftzVm_cKtcKKIXCQF2SBQqhSS2CXZAGAq1JTgdfkJuevc-Urzhakqoufg-3iaMd49EUeD-5U9KEYUj_0aYz93nbF3h7jp53KLbkKtsv-7i-X5ONps1u_lNu359d1vS1bKnEspQSK0llHER00ymIAZJIJyZywgWvfovAONAaKXEsllW10w3Xr0Vnu2JLA_NumPufkgxlS_LbpZBDM5GsmXzP5mtn3jDzMSPTe_885AlOKsl_XXFDn</recordid><startdate>197107</startdate><enddate>197107</enddate><creator>Guelman, Mauricio</creator><general>IEEE</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>197107</creationdate><title>A qualitative study of proportional navigation</title><author>Guelman, Mauricio</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c261t-660216dad211d0b7a1f01363563d5af49ec15ed091f21496767ab9b49ce1da4d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1971</creationdate><topic>Aerodynamics</topic><topic>Differential equations</topic><topic>Geometry</topic><topic>Kinematics</topic><topic>Missiles</topic><topic>Navigation</topic><topic>Proportional control</topic><topic>Time varying systems</topic><topic>Trajectory</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Guelman, Mauricio</creatorcontrib><collection>CrossRef</collection><jtitle>IEEE transactions on aerospace and electronic systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Guelman, Mauricio</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A qualitative study of proportional navigation</atitle><jtitle>IEEE transactions on aerospace and electronic systems</jtitle><stitle>T-AES</stitle><date>1971-07</date><risdate>1971</risdate><volume>AES-7</volume><issue>4</issue><spage>637</spage><epage>643</epage><pages>637-643</pages><issn>0018-9251</issn><eissn>1557-9603</eissn><coden>IEARAX</coden><abstract>This paper represents a study of the trajectories of an ideal missile homing on a target according to the proportional navigation law. 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| identifier | ISSN: 0018-9251 |
| ispartof | IEEE transactions on aerospace and electronic systems, 1971-07, Vol.AES-7 (4), p.637-643 |
| issn | 0018-9251 1557-9603 |
| language | eng |
| recordid | cdi_ieee_primary_4103772 |
| source | IEEE Electronic Library (IEL) |
| subjects | Aerodynamics Differential equations Geometry Kinematics Missiles Navigation Proportional control Time varying systems Trajectory |
| title | A qualitative study of proportional navigation |
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