The air of this work is study possibility of caring out inspection maneuvers of International Space Station (ISS) using Spacecraft-Inspector (SCI) that equipped with electric propulsion system. We study simple maneuvers – distinction SCI from ISS and transferring SCI to stationary point, circumnavigation transfer to ellipse or point. Motion is studies in orbital cylindrical reference frame. Control programs defined in linearized model of motion. Numerical simulation of relative motion carried out in original model taking into account atmospheric perturbation.


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    Titel :

    Ballistic analyze of spacecraft inspector motion, equipped with electric thruster, above International Space Station


    Beteiligte:

    Kongress:

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


    Erschienen in:

    Erscheinungsdatum :

    04.12.2018


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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