METHOD OF DISCHARGING POWER FROM GYRO OF SPACECRAFT WITH CREATING THE MAGNETIC MOMENT Russian patent published in 2016 - IPC B64G1/28 H01Q21/06

Abstract RU 2580593 C2

FIELD: spacecraft.

SUBSTANCE: invention relates to controlling the angular movement of the spacecraft. For unloading the system of power gyroscopes from angular momentum current loops of a phased array (PAR) are used. According to the magnetic moments of these circuits the total value of the magnetic moment of the PAR in each mode of its operation is determined. Then the unloading point is calculated, generated by the interaction of the magnetic moments by PAR with Earth's magnetic field. When the condition of discharge is met determine the appropriate mode of operation PAR with the required discharge point and conduct discharge.

EFFECT: technical result of the invention is to improve the efficiency of discharge of power gyroscopes.

1 cl, 5 dwg

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RU 2 580 593 C2

Authors

Kovtun Vladimir Semenovich

Frolov Igor Vladimirovich

Ermakov Petr Nikolaevich

Dates

2016-04-10—Published

2014-06-10—Filed