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
2009
Article (Journal)
English
BKL: | 55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung | |
Local classification TIB: | 770/3520/8000 |
Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit
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