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Design of The Topsat Mission

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dc.contributor.author Vincent, Mark A. en_US
dc.date.accessioned 2004-10-06T04:40:00Z
dc.date.available 2004-10-06T04:40:00Z
dc.date.issued 1993-08-16 en_US
dc.identifier.citation Victoria, B.C., Canada en_US
dc.identifier.clearanceno 93-1435 en_US
dc.identifier.uri http://hdl.handle.net/2014/35711
dc.description.abstract The currently preferred design for a global topography satellite mission poses a challenging task in orbit design and navigation since it requires close formation flying of two rada antenna equipped satellites. This paper describes the origin of the orbital requirements and some methods to achieve success. en_US
dc.format.extent 343438 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Topsat Design global topography en_US
dc.title Design of The Topsat Mission en_US


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