Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit

Details Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit

Jun 2009

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2009cosre..47..243p&link_type=abstract

Cosmic Research, Volume 47, Issue 3, pp.243-250

Physics

45.40.Gj

Scientific paper

The results of numerical optimization of multi-orbit trajectories of the transfer of a low-thrust spacecraft to a high elliptic orbit are presented. An analysis of characteristics of the optimal transfers including their structure is performed. The methods of description of the structures of optimal multi-orbit trajectories are suggested with the goal of their classification.

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