dc.contributor.author | Sharaf, M.A. | |
dc.contributor.author | Alshaary, A. A. | |
dc.date.accessioned | 2018-07-22T10:28:02Z | |
dc.date.available | 2018-07-22T10:28:02Z | |
dc.date.issued | 2008-01-01 | |
dc.identifier.issn | 1815-3852 | |
dc.identifier.uri | https://journal.uob.edu.bh:443/handle/123456789/453 | |
dc.description.abstract | In the present paper, use will be made of Thorne's series solution of Lambert problem to develop an orbit determination method valid for hyperbolic and elliptical orbits. Numerical illustrations are given. | en_US |
dc.language.iso | en | en_US |
dc.publisher | University of Bahrain | en_US |
dc.rights | Attribution-NonCommercial-ShareAlike 4.0 International | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-sa/4.0/ | * |
dc.subject | Orbit determination | en_US |
dc.subject | Lambert problem | en_US |
dc.subject | Space dynamics | en_US |
dc.title | Orbit Determination Method Using Thorne's Series Solution of Lambert Problem | en_US |
dc.type | Article | en_US |
dc.source.title | Arab Journal of Basic and Applied Sciences | |
dc.abbreviatedsourcetitle | AJBAS |
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