The size of collision solutions in orbital elements space

The size of collision solutions in orbital elements space

In the framework of the analytical theory of close encounters, and under suitable assumptions, we compute the size of the region in orbital elements space containing collisions solutions. In the linearized approximation in the semimajor axis/eccentricity plane the collision region is the interior of...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Proceedings of the International Astronomical Union 2004-08, Vol.2004 (IAUC197), p.249-254
Hauptverfasser: Valsecchi, G.B., Rossi, A., Milani, A., Chesley, S.R.
Format: Artikel
Sprache:eng
Schlagworte:
Contributed Papers
Earth
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 254
container_issue IAUC197
container_start_page 249
container_title Proceedings of the International Astronomical Union
container_volume 2004
creator Valsecchi, G.B.
Rossi, A.
Milani, A.
Chesley, S.R.
description In the framework of the analytical theory of close encounters, and under suitable assumptions, we compute the size of the region in orbital elements space containing collisions solutions. In the linearized approximation in the semimajor axis/eccentricity plane the collision region is the interior of an ellipse. Examples are given from past cases of Near Earth Asteroids having the possibility of impacting our planet.To search for other articles by the author(s) go to: http://adsabs.harvard.edu/abstract_service.html
doi_str_mv 10.1017/S1743921304008725
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_225174830</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><cupid>10_1017_S1743921304008725</cupid><sourcerecordid>1400564341</sourcerecordid><originalsourceid>FETCH-LOGICAL-c359t-bffd0e67699280e73748705d4f404fbe159a415f68de5b16c27dbbc067f07c643</originalsourceid><addsrcrecordid>eNp1kEtPwzAQhC0EEqXwA7hZ3APrd3xEFS-pEgfKOUqcNbhK4mKnB_j1pGoFB8RpR6v5ZrVDyCWDawbM3LwwI4XlTIAEKA1XR2S2WxWWc3b8o5k4JWc5rwGkLoWaEbt6R5rDF9LoqYtdF3KIA82x246TyDQMNKYmjHVHscMehzHTvKkdnpMTX3cZLw5zTl7v71aLx2L5_PC0uF0WTig7Fo33LaA22lpeAhphZGlAtdJLkL5BpmwtmfK6bFE1TDtu2qZxoI0H47QUc3K1z92k-LHFPFbruE3DdLLiXE1_lQImE9ubXIo5J_TVJoW-Tp8Vg2pXUPWnoIkRB6bumxTaN_xN_p_6BgUkZng</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>225174830</pqid></control><display><type>article</type><title>The size of collision solutions in orbital elements space</title><source>Cambridge University Press Journals Complete</source><creator>Valsecchi, G.B. ; Rossi, A. ; Milani, A. ; Chesley, S.R.</creator><creatorcontrib>Valsecchi, G.B. ; Rossi, A. ; Milani, A. ; Chesley, S.R.</creatorcontrib><description>In the framework of the analytical theory of close encounters, and under suitable assumptions, we compute the size of the region in orbital elements space containing collisions solutions. In the linearized approximation in the semimajor axis/eccentricity plane the collision region is the interior of an ellipse. Examples are given from past cases of Near Earth Asteroids having the possibility of impacting our planet.To search for other articles by the author(s) go to: http://adsabs.harvard.edu/abstract_service.html</description><identifier>ISSN: 1743-9213</identifier><identifier>EISSN: 1743-9221</identifier><identifier>DOI: 10.1017/S1743921304008725</identifier><language>eng</language><publisher>Cambridge, UK: Cambridge University Press</publisher><subject>Contributed Papers ; Earth</subject><ispartof>Proceedings of the International Astronomical Union, 2004-08, Vol.2004 (IAUC197), p.249-254</ispartof><rights>2005 International Astronomical Union</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c359t-bffd0e67699280e73748705d4f404fbe159a415f68de5b16c27dbbc067f07c643</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.cambridge.org/core/product/identifier/S1743921304008725/type/journal_article$$EHTML$$P50$$Gcambridge$$H</linktohtml><link.rule.ids>164,314,776,780,27901,27902,55603</link.rule.ids></links><search><creatorcontrib>Valsecchi, G.B.</creatorcontrib><creatorcontrib>Rossi, A.</creatorcontrib><creatorcontrib>Milani, A.</creatorcontrib><creatorcontrib>Chesley, S.R.</creatorcontrib><title>The size of collision solutions in orbital elements space</title><title>Proceedings of the International Astronomical Union</title><addtitle>Proc. IAU</addtitle><description>In the framework of the analytical theory of close encounters, and under suitable assumptions, we compute the size of the region in orbital elements space containing collisions solutions. In the linearized approximation in the semimajor axis/eccentricity plane the collision region is the interior of an ellipse. Examples are given from past cases of Near Earth Asteroids having the possibility of impacting our planet.To search for other articles by the author(s) go to: http://adsabs.harvard.edu/abstract_service.html</description><subject>Contributed Papers</subject><subject>Earth</subject><issn>1743-9213</issn><issn>1743-9221</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2004</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNp1kEtPwzAQhC0EEqXwA7hZ3APrd3xEFS-pEgfKOUqcNbhK4mKnB_j1pGoFB8RpR6v5ZrVDyCWDawbM3LwwI4XlTIAEKA1XR2S2WxWWc3b8o5k4JWc5rwGkLoWaEbt6R5rDF9LoqYtdF3KIA82x246TyDQMNKYmjHVHscMehzHTvKkdnpMTX3cZLw5zTl7v71aLx2L5_PC0uF0WTig7Fo33LaA22lpeAhphZGlAtdJLkL5BpmwtmfK6bFE1TDtu2qZxoI0H47QUc3K1z92k-LHFPFbruE3DdLLiXE1_lQImE9ubXIo5J_TVJoW-Tp8Vg2pXUPWnoIkRB6bumxTaN_xN_p_6BgUkZng</recordid><startdate>20040801</startdate><enddate>20040801</enddate><creator>Valsecchi, G.B.</creator><creator>Rossi, A.</creator><creator>Milani, A.</creator><creator>Chesley, S.R.</creator><general>Cambridge University Press</general><scope>AAYXX</scope><scope>CITATION</scope><scope>3V.</scope><scope>7XB</scope><scope>88I</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>GNUQQ</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>M2P</scope><scope>P5Z</scope><scope>P62</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>Q9U</scope></search><sort><creationdate>20040801</creationdate><title>The size of collision solutions in orbital elements space</title><author>Valsecchi, G.B. ; Rossi, A. ; Milani, A. ; Chesley, S.R.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c359t-bffd0e67699280e73748705d4f404fbe159a415f68de5b16c27dbbc067f07c643</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2004</creationdate><topic>Contributed Papers</topic><topic>Earth</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Valsecchi, G.B.</creatorcontrib><creatorcontrib>Rossi, A.</creatorcontrib><creatorcontrib>Milani, A.</creatorcontrib><creatorcontrib>Chesley, S.R.</creatorcontrib><collection>CrossRef</collection><collection>ProQuest Central (Corporate)</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Science Database (Alumni Edition)</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies &amp; Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>ProQuest Central Student</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Science Database</collection><collection>Advanced Technologies &amp; Aerospace Database</collection><collection>ProQuest Advanced Technologies &amp; Aerospace Collection</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>ProQuest Central Basic</collection><jtitle>Proceedings of the International Astronomical Union</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Valsecchi, G.B.</au><au>Rossi, A.</au><au>Milani, A.</au><au>Chesley, S.R.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>The size of collision solutions in orbital elements space</atitle><jtitle>Proceedings of the International Astronomical Union</jtitle><addtitle>Proc. IAU</addtitle><date>2004-08-01</date><risdate>2004</risdate><volume>2004</volume><issue>IAUC197</issue><spage>249</spage><epage>254</epage><pages>249-254</pages><issn>1743-9213</issn><eissn>1743-9221</eissn><abstract>In the framework of the analytical theory of close encounters, and under suitable assumptions, we compute the size of the region in orbital elements space containing collisions solutions. In the linearized approximation in the semimajor axis/eccentricity plane the collision region is the interior of an ellipse. Examples are given from past cases of Near Earth Asteroids having the possibility of impacting our planet.To search for other articles by the author(s) go to: http://adsabs.harvard.edu/abstract_service.html</abstract><cop>Cambridge, UK</cop><pub>Cambridge University Press</pub><doi>10.1017/S1743921304008725</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 1743-9213
ispartof Proceedings of the International Astronomical Union, 2004-08, Vol.2004 (IAUC197), p.249-254
issn 1743-9213
1743-9221
language eng
recordid cdi_proquest_journals_225174830
source Cambridge University Press Journals Complete
subjects Contributed Papers
Earth
title The size of collision solutions in orbital elements space
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-09T07%3A06%3A54IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=The%20size%20of%20collision%20solutions%20in%20orbital%20elements%20space&rft.jtitle=Proceedings%20of%20the%20International%20Astronomical%20Union&rft.au=Valsecchi,%20G.B.&rft.date=2004-08-01&rft.volume=2004&rft.issue=IAUC197&rft.spage=249&rft.epage=254&rft.pages=249-254&rft.issn=1743-9213&rft.eissn=1743-9221&rft_id=info:doi/10.1017/S1743921304008725&rft_dat=%3Cproquest_cross%3E1400564341%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=225174830&rft_id=info:pmid/&rft_cupid=10_1017_S1743921304008725&rfr_iscdi=true