The utility model relates to a high precision velocity-
mode control system of a
magnetic levitation counteractive
flywheel motor, which is used in a high precision
attitude control executive device of a new-generation
satellite with high-stability, namely the high precision velocity controlling of the
magnetic levitation counteractive
flywheel motor. The utility model mainly comprises a controller with a DSP as the core, a three-phase bridge power
amplifier, a three-phase bridge drive circuit, an increment type shaft angle
encoder, a three-phase permanent magnetic brushless
direct current motor, a 28V steady
direct current power supply, a +15V steady
direct current power supply, a plus or minus 5V steady direct current power supply, a current checking part and Hall-effect rotor
position sensor. Through the two channels of orthogonal encoding pulse
signal of the increment type shaft angle
encoder, the utility model provides the low-velocity controlling of the
magnetic levitation counteractive
flywheel motor with the
velocity feedback when the velocity is in the electrically allowable rotational speed range of the increment type shaft angle
encoder to realize the high precision velocity-mode controlling of the magnetic
levitation counteractive flywheel motor; the
signal of the Hall-effect rotor
position sensor is used as the
velocity feedback when the velocity is out of the electrically allowable rotational speed range of the increment type shaft angle encoder.