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dc.contributor.authorPetroškevičius, Petras
dc.date.accessioned2023-09-18T18:38:31Z
dc.date.available2023-09-18T18:38:31Z
dc.date.issued2001
dc.identifier.issn1392-1541
dc.identifier.other(BIS)VGT02-000002800
dc.identifier.urihttps://etalpykla.vilniustech.lt/handle/123456789/130021
dc.description.abstractFor research of the Earth’s gravitational field, for determining geocentric coordinates and for solving other satellite geodesy tasks by dynamic method most often Earth’s satellites moving in almost circular orbits are used. For research of the Earth’s gravitational field the continued orbits with eccentricity close to 1 are used. Satellites’ moving in continued orbits usage is complicated due to satellite coordinates and their function series, whose absolute convergence until eccentricity e reaches Laplace’s limit (0.6627). Such usage could be extended by using satellite coordinates power of series size, which absolutely converge at eccentricity values from 0 to 1. Satellites moving in almost parabolic orbits are farther from the Earth and are more influenced by the Moon, the Sun and other celestial bodies. [...].eng
dc.format.extentp. 152-156
dc.format.mediumtekstas / txt
dc.language.isolit
dc.titleDangaus kūno gravitacinio poveikio trikdančiosios funkcijos reiškimas laipsnine eilute
dc.title.alternativePresentation of celestial body gravitational influence perturbation function by power series
dc.typeStraipsnis kitame recenzuotame leidinyje / Article in other peer-reviewed source
dc.type.pubtypeS4 - Straipsnis kitame recenzuotame leidinyje / Article in other peer-reviewed publication
dc.contributor.institutionVilniaus Gedimino technikos universitetas
dc.contributor.facultyAplinkos inžinerijos fakultetas / Faculty of Environmental Engineering
dc.subject.researchfieldT 010 - Matavimų inžinerija / Measurement engineering
dcterms.sourcetitleGeodezija ir kartografija
dc.description.issueNr. 4
dc.description.volumeT. XXVII
dc.publisher.nameTechnika
dc.publisher.cityVilnius
dc.identifier.elaba3584983


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