FIELD: electrical engineering.
SUBSTANCE: invention relates to the field of electric engineering, in particular, to astatic control systems of dynamic moments of flywheel control motor (FCM), made on the basis of synchronous motor with permanent magnets, used as electromechanical actuators of spacecraft orientation and stabilization systems. Control method of dynamic moment of control engine-flywheel includes engine rpm controller, rotor position sensor, sine-cosine reference frequency generator, multipliers, pulse signal former, dynamic moment control signal integrator to generate engine flywheel reference frequency, converter of signals from rotor position sensor into digital code of current speed of engine-flywheel and digital adder, which determines difference signal of setting and current frequency.
EFFECT: technical result, to which achievement proposed invention is aimed, is reduction of harmonic signals transformations number, due to which it is possible to achieve increase in quick action of control loop and simplification of electric drive structure at control of dynamic moment of engine-flywheel, which leads to reduction of its weight and increase in reliability.
1 cl, 2 dwg
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Authors
Dates
2020-11-17—Published
2020-05-13—Filed