SYNTHESIS OF A SPACE CRAFT’S ROTARY MOTION MODEL SUBJECT                                        TO THE MAGNETIC FIELD AND ATMOSPHERE OF THE EARTH

Tulekenova Dana Toleubekovna, assistant, sub-department of systems for administration of aerospace technology, Almaty university of power engineering and connection (050013, 126 Baytursynova street, Almaty,Kazakhstan), aipet@aipet.kz, dana_tul@mail.ru
Ergaliev Dastan Syrymovich, candidate of technical sciences, associate professor, professor, sub-department of space engineering and technology, Eurasian National University named after L. N. Gumilyov (010000, 2 Satpaeva street, Astana, Kazahstan), eds_kaz67@mail.ru
Tulegulov Amandos Dabysovich, candidate of physical and mathematical sciences, associate professor, head of sub-department of space engineering and technology, Eurasian National University named after L. N. Gumilyov (010000, 2 Satpaeva street, Astana, Kazahstan), TAD62@ya.ru
Ibraev Olzhas Serikzhanovich, lecturer, sub-department of space engineering and technology, Eurasian National University named after L. N. Gumilyov (010000, 2 Satpaeva street, Astana, Kazahstan), 7701276767695@yandex.kz

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Numerical calculations determining the parameters of the rotational motion of the spacecraft in orbital coordinate system with the magnetic field and the Earth's atmosphere for inclined orbits.

method, extensional, intensional, multidimensional test, expert knowledge, scale, prototype, diagnostics, expert, indication, space.