Analytical methods for satellite constellation reconfiguration and reconnaissance using low-thrust manoeuvres
A fully-analytical general perturbation solution to a restricted low-thrust circular to circular Lambert rendezvous problem with tangential thrust and an optional coast arc is developed. The solution requires no iteration and is solved rapidly to generate a full range of possible manoeuvres to achie...
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University of Strathclyde
2018
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| Online Access: | https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.759456 |