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.
Ballistic analyze of spacecraft inspector motion, equipped with electric thruster, above International Space Station
ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia
AIP Conference Proceedings ; 2046 , 1
04.12.2018
10 pages
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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