The problem of the formation of an optimal control program spacecraft with low thrust at flight between the noncoplanar elliptical and geostationary orbits is considered. A scheme for the joint change of orbital elements within the simple structure of the thrust vector control on the circuit is offered.


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    Title :

    Optimum program of control of continuous low-thrust at flight between noncoplanar elliptical and geostationary orbits


    Contributors:

    Conference:

    ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia


    Published in:

    Publication date :

    2018-12-04


    Size :

    6 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English