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.