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.


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    Title :

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


    Contributors:

    Published in:

    Cosmic Research ; 47 , 3 ; 243-250


    Publication date :

    2009-06-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English