DETERMINATION OF THE ORBITAL PARAMETERS OF ARTIFICIAL SATELLITES ON THE BASIS OF OBSERVATIONS FROM THE EARTH'S SURFACE
Methods are presented for the determination of the orbital elements of a satellite and of the analysis of its motion on the basis of the processing of optical and radar observation data. The methods are designed for the utilization of high speed electronic computing machines. (Author) Trans. of Isku...
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creator | ENEEV,T M Platonov,A K Kazakova,P K |
description | Methods are presented for the determination of the orbital elements of a satellite and of the analysis of its motion on the basis of the processing of optical and radar observation data. The methods are designed for the utilization of high speed electronic computing machines. (Author)
Trans. of Iskusstvennye Sputniki Zemli (USSR) v4 p43-55 1960. |
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Trans. of Iskusstvennye Sputniki Zemli (USSR) v4 p43-55 1960.</description><language>eng</language><subject>ARTIFICIAL SATELLITES ; CELESTIAL MECHANICS ; ITERATIONS ; MATHEMATICAL PREDICTION ; MATRICES(MATHEMATICS) ; OPTICAL TRACKING ; ORBITS ; PARTIAL DIFFERENTIAL EQUATIONS ; RADAR TRACKING ; TRACKING</subject><creationdate>1961</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0615400$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ENEEV,T M</creatorcontrib><creatorcontrib>Platonov,A K</creatorcontrib><creatorcontrib>Kazakova,P K</creatorcontrib><creatorcontrib>LAND-AIR INC POINT MUGU CALIF</creatorcontrib><title>DETERMINATION OF THE ORBITAL PARAMETERS OF ARTIFICIAL SATELLITES ON THE BASIS OF OBSERVATIONS FROM THE EARTH'S SURFACE</title><description>Methods are presented for the determination of the orbital elements of a satellite and of the analysis of its motion on the basis of the processing of optical and radar observation data. The methods are designed for the utilization of high speed electronic computing machines. (Author)
Trans. of Iskusstvennye Sputniki Zemli (USSR) v4 p43-55 1960.</description><subject>ARTIFICIAL SATELLITES</subject><subject>CELESTIAL MECHANICS</subject><subject>ITERATIONS</subject><subject>MATHEMATICAL PREDICTION</subject><subject>MATRICES(MATHEMATICS)</subject><subject>OPTICAL TRACKING</subject><subject>ORBITS</subject><subject>PARTIAL DIFFERENTIAL EQUATIONS</subject><subject>RADAR TRACKING</subject><subject>TRACKING</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1961</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFzL0KwkAQBOA0FqK-gcV1VkLEn37vssctJDnZXW2DaISA2CT4_CaHvdUU38zMs0-BilxRDUqxNtEbDWgiW1IozRkYqqkgkwAreXI0goBiWZLiCHWaWBBKrWgF-ZruxHiOVWIcx2EjRi7sweEymz1vr75d_XKRrT2qC9vH0N2bfuje7dBAkZ92x0Oe7__wF9fENjg</recordid><startdate>19610315</startdate><enddate>19610315</enddate><creator>ENEEV,T M</creator><creator>Platonov,A K</creator><creator>Kazakova,P K</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19610315</creationdate><title>DETERMINATION OF THE ORBITAL PARAMETERS OF ARTIFICIAL SATELLITES ON THE BASIS OF OBSERVATIONS FROM THE EARTH'S SURFACE</title><author>ENEEV,T M ; Platonov,A K ; Kazakova,P K</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD06154003</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1961</creationdate><topic>ARTIFICIAL SATELLITES</topic><topic>CELESTIAL MECHANICS</topic><topic>ITERATIONS</topic><topic>MATHEMATICAL PREDICTION</topic><topic>MATRICES(MATHEMATICS)</topic><topic>OPTICAL TRACKING</topic><topic>ORBITS</topic><topic>PARTIAL DIFFERENTIAL EQUATIONS</topic><topic>RADAR TRACKING</topic><topic>TRACKING</topic><toplevel>online_resources</toplevel><creatorcontrib>ENEEV,T M</creatorcontrib><creatorcontrib>Platonov,A K</creatorcontrib><creatorcontrib>Kazakova,P K</creatorcontrib><creatorcontrib>LAND-AIR INC POINT MUGU CALIF</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ENEEV,T M</au><au>Platonov,A K</au><au>Kazakova,P K</au><aucorp>LAND-AIR INC POINT MUGU CALIF</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>DETERMINATION OF THE ORBITAL PARAMETERS OF ARTIFICIAL SATELLITES ON THE BASIS OF OBSERVATIONS FROM THE EARTH'S SURFACE</btitle><date>1961-03-15</date><risdate>1961</risdate><abstract>Methods are presented for the determination of the orbital elements of a satellite and of the analysis of its motion on the basis of the processing of optical and radar observation data. The methods are designed for the utilization of high speed electronic computing machines. (Author)
Trans. of Iskusstvennye Sputniki Zemli (USSR) v4 p43-55 1960.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | ARTIFICIAL SATELLITES CELESTIAL MECHANICS ITERATIONS MATHEMATICAL PREDICTION MATRICES(MATHEMATICS) OPTICAL TRACKING ORBITS PARTIAL DIFFERENTIAL EQUATIONS RADAR TRACKING TRACKING |
title | DETERMINATION OF THE ORBITAL PARAMETERS OF ARTIFICIAL SATELLITES ON THE BASIS OF OBSERVATIONS FROM THE EARTH'S SURFACE |
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