Please use this identifier to cite or link to this item: http://hdl.handle.net/2248/7886
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dc.contributor.authorVyasanakere, Jayanth P-
dc.contributor.authorBhatnagar, Siddharth-
dc.contributor.authorMurthy, J-
dc.date.accessioned2021-12-16T04:06:15Z-
dc.date.available2021-12-16T04:06:15Z-
dc.date.issued2021-12-
dc.identifier.citationPramana Journal of Physics, Vol. 95, No. 4, 192en_US
dc.identifier.issn0304-4289-
dc.identifier.urihttp://hdl.handle.net/2248/7886-
dc.descriptionRestricted Accessen_US
dc.descriptionThe original publication is available at springerlink.com-
dc.description.abstractWe describe a method that does not use any orbital parameters, to arrive at the position and mass of a new celestial object, using high-precision orbital state vector data of the rest of the objects in the system. As an illustration of this approach, we rediscover Neptune with remarkable accuracy.en_US
dc.language.isoenen_US
dc.publisherSpringeren_US
dc.relation.urihttps://doi.org/10.1007/s12043-021-02238-2-
dc.rights© Indian Academy of Sciences-
dc.subjectNon-parametric algorithen_US
dc.subjectNeptuneen_US
dc.subjectiteration methoden_US
dc.titleDiscovering a celestial object using a non-parametric algorithmen_US
dc.typeArticleen_US
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