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  5. Complex methodology of the satellite attitude control system executive bodies

Complex methodology of the satellite attitude control system executive bodies

A.S. Nazarov
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The article is devoted to the complex methodology of the executive bodies, within which proposed and implemented methods: calming of satellite at incomplete dirigibility; unloading of inertia fly-wheels by means of gyros; turn satellite at incomplete dirigibility; choice of model parameters and forming of control moments of kinematics satellite model.
Keywords: executive body, calming of satellite, incomplete dirigibility, unloading inertial flywheel, power gyro complex, attitude control system