Orbit Determination Method Using Thorne's Series Solution of Lambert Problem

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