Semi-analytical solution for the optimal low-thrust deflection of Near-Earth Objects: Efficient robust opimisation for space mission design in the frame of evidence theory

Croisard, C., Vasile, M. and Radice, G. (2009) Semi-analytical solution for the optimal low-thrust deflection of Near-Earth Objects: Efficient robust opimisation for space mission design in the frame of evidence theory. In: 60tj International Astronautical Congress, Daejeon, South Korea, 12-16 Oct 2009,

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Item Type:Conference Proceedings
Status:Published
Refereed:Yes
Glasgow Author(s) Enlighten ID:Radice, Dr Gianmarco and Vasile, Dr Massimiliano
Authors: Croisard, C., Vasile, M., and Radice, G.
College/School:College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity
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