The invention discloses a frame
system for a
control moment gyroscope. The frame
system can be used as a posture control executing mechanism of large
spacecraft like a large
satellite and a space
station and is composed of a
rotary transformer end mechanical bearing, a conducting slide ring, a
rotary transformer, a
rotary transformer base, a rotary variable shaft, a
harmonic shaft, a frame, a motor base, a
harmonic reducer, a frame motor
stator assembly, a frame motor rotor
assembly, a motor end mechanical bearing and the like. A frame core shaft is driven by a frame moment motor to drive a connected
gyroscope rotor to rotate to output
gyroscope moment, the rotary
transformer is in charge of outputting an angular position
signal of the frame core shaft to be fed back to a
control system ofa moment motor, therefore the moment motor is controlled, an iron core fractional slot structure is adopted by the moment motor to reduce flux leakage, after the moment output by the motor is amplified by the
harmonic reducer, the moment is transferred to the
gyroscope rotor, and therefore, gyroscope torque is output. The frame
system has the advantages that the
layout is compact, the size is small, the weight is low, the system
noise is small, and the control precision and torque output efficiency of the frame system are high.