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MATHEMATICAL MODELING OF MOVEMENT SMALL SPACECRAFT AROUND THE MASS CENTER IN THE COMPOSITION OF ORBITAL DEPLOY TETHER SYSTEM
Ulyanov Nikita Vladimirovich
Samara State Aerospace University named after academician S.P. Korolev (National Research University)
Student of the Faculty of Informatics
Samara State Aerospace University named after academician S.P. Korolev (National Research University)
Student of the Faculty of Informatics
Abstract
A model of movement small spacecraft around the mass center in the composition of orbital deployment tether system. The aim of this work is to study the dynamics of motion of the small spacecraft with arbitrary inertia tensor.
Keywords: inertia tensor, mathematical modeling, orbital tether system, spacecraft, the equations of motion
Category: 01.00.00 Physics and mathematics
Article reference:
Mathematical modeling of movement small spacecraft around the mass center in the composition of orbital deploy tether system // Modern scientific researches and innovations. 2016. № 4 [Electronic journal]. URL: https://web.snauka.ru/en/issues/2016/04/67340
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