Konferans bildirisi Açık Erişim
Imre, Egemen; Palmer, Philip L.
<?xml version='1.0' encoding='UTF-8'?> <record xmlns="http://www.loc.gov/MARC21/slim"> <leader>00000nam##2200000uu#4500</leader> <datafield tag="700" ind1=" " ind2=" "> <subfield code="a">Palmer, Philip L.</subfield> <subfield code="u">Univ Surrey, Surrey Space Ctr, Surrey, England</subfield> </datafield> <datafield tag="980" ind1=" " ind2=" "> <subfield code="a">user-tubitak-destekli-proje-yayinlari</subfield> </datafield> <datafield tag="540" ind1=" " ind2=" "> <subfield code="a">Creative Commons Attribution</subfield> <subfield code="u">http://www.opendefinition.org/licenses/cc-by</subfield> </datafield> <datafield tag="773" ind1=" " ind2=" "> <subfield code="i">isVersionOf</subfield> <subfield code="a">10.81043/aperta.110943</subfield> <subfield code="n">doi</subfield> </datafield> <datafield tag="024" ind1=" " ind2=" "> <subfield code="a">10.81043/aperta.110944</subfield> <subfield code="2">doi</subfield> </datafield> <datafield tag="245" ind1=" " ind2=" "> <subfield code="a">A numerical approach to high precision relative orbit propagation</subfield> </datafield> <datafield tag="100" ind1=" " ind2=" "> <subfield code="a">Imre, Egemen</subfield> <subfield code="u">Univ Surrey, Surrey Space Ctr, Surrey, England</subfield> </datafield> <datafield tag="909" ind1="C" ind2="O"> <subfield code="o">oai:zenodo.org:110944</subfield> <subfield code="p">user-tubitak-destekli-proje-yayinlari</subfield> </datafield> <datafield tag="650" ind1="1" ind2="7"> <subfield code="2">opendefinition.org</subfield> <subfield code="a">cc-by</subfield> </datafield> <datafield tag="260" ind1=" " ind2=" "> <subfield code="c">2006-01-01</subfield> </datafield> <datafield tag="856" ind1="4" ind2=" "> <subfield code="u">https://aperta.ulakbim.gov.trrecord/110944/files/bib-7d4ba32f-d310-4bc5-a082-985fe70a572b.txt</subfield> <subfield code="z">md5:9d4ac7346328b4fa99c0d14a94ef4e90</subfield> <subfield code="s">133</subfield> </datafield> <datafield tag="542" ind1=" " ind2=" "> <subfield code="l">open</subfield> </datafield> <controlfield tag="005">20210420141416.0</controlfield> <controlfield tag="001">110944</controlfield> <datafield tag="980" ind1=" " ind2=" "> <subfield code="a">publication</subfield> <subfield code="b">conferencepaper</subfield> </datafield> <datafield tag="711" ind1=" " ind2=" "> <subfield code="a">ASTRODYNAMICS 2005, VOL 123, PTS 1-3</subfield> </datafield> <datafield tag="520" ind1=" " ind2=" "> <subfield code="a">This paper presents a numerical method to propagate relative orbits which can handle up to an arbitrary number of zonal and tesseral geopotential terms and can be extended to accommodate the effects of atmospheric drag. This method relies on defining a 'relative Hamiltonian,' which describes both the absolute and the relative motion of two satellites. Exploiting the separability of the solution, the Keplerian motion is described via analytical means whereas the effects of higher order terms are handled via a symplectic numerical integration scheme. The derivation and the numerical integration are designed to conserve the constants of the motion, resulting in better long term accuracy.</subfield> </datafield> </record>
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