The problem of optimization of interplanetary low-thrust trajectories using gravity assist maneuvers is considered. The mathematical model of gravity assist maneuver, necessary conditions of optimality of trajectory with gravity assist maneuvers and description of continuation method for solving the problem of optimization of low-thrust interplanetary trajectory using gravity assist maneuvers are given. Numerical examples of optimal trajectories are presented.


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    Title :

    Optimization of Complex Schemes of Interplanetary Low Thrust Transfers


    Additional title:

    Studies in Systems, Decision and Control


    Contributors:


    Publication date :

    2025-05-29


    Size :

    21 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English