Orbital perturbations using geopotential coefficients up to high degree and order: Highly eccentric orbits

dc.contributor.authorDe Moraes, Rodolpho Vilhena [UNESP]
dc.contributor.authorWnuk, Edwin
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)
dc.contributor.institutionAdam Mickiewicz University
dc.date.accessioned2022-04-28T19:56:30Z
dc.date.available2022-04-28T19:56:30Z
dc.date.issued1998-12-01
dc.description.abstractSeveral methods have been proposed for calculations of the eccentricity function for a high value of the eccentricity, however they cannot be used when the high degree and order coefficients of gravity fields are taken into account. The method proposed by Wnuk1 is numerically stable in this case, but when is used, a large number of terms occurs in formulas for geopotential perturbations. In this paper we propose an application of expansions of some functions of the eccentric anomaly E as well as Hansen coefficients in power series of (e - e*), where e* is a fixed value of the eccentricity derived by Da Silva Fernandes2,3,4. These series are convergent for all e < 1.en
dc.description.affiliationGrupo Dinemica Orbital Planetologia DMA-FEG-UNESP, 12500-000, Guaratinguetá, SP
dc.description.affiliationAstronomical Observatory Adam Mickiewicz University, ul. Sloneczna 36, 60-286 Poznan
dc.description.affiliationUnespGrupo Dinemica Orbital Planetologia DMA-FEG-UNESP, 12500-000, Guaratinguetá, SP
dc.format.extent227-238
dc.identifier.citationAdvances in the Astronautical Sciences, v. 100, n. 1, p. 227-238, 1998.
dc.identifier.issn0065-3438
dc.identifier.scopus2-s2.0-0346877290
dc.identifier.urihttp://hdl.handle.net/11449/224428
dc.language.isoeng
dc.relation.ispartofAdvances in the Astronautical Sciences
dc.sourceScopus
dc.titleOrbital perturbations using geopotential coefficients up to high degree and order: Highly eccentric orbitsen
dc.typeArtigo

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