Precise orbit determination and analysis from satellite altimetry and laser ranging
For optimum utilization of satellite-borne instrumentation, it is necessary to know precisely the orbital position of the spacecraft. The aim of this thesis is therefore two-fold - firstly to derive precise orbits with particular emphasis placed on the altimetric satellite SEASAT and secondly, to ut...
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Aston University
1989
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| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.253710 |