The problem of control laws, allowing the formation and maintenance of the required halo-orbit, is considered. The motion of the electric propulsion spacecraft is considered in the vicinity of the collinear libration points of the Earth-Moon system. The gravitational effects of the Earth, the Moon and the Sun are taken into account. The results are based on the simplified linearized models of the gravitational potential.


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    Title :

    Halo-orbit formation in the Earth-Moon system by the electric propulsion spacecraft


    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 :

    8 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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