Abstract 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.
Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit
Cosmic Research ; 47 , 3 ; 243-250
2009-06-01
8 pages
Article (Journal)
Electronic Resource
English
Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit
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