Satellites need movable parts to function, including attitude-controlling reaction flywheels, control moment gyroscopes, reaction jet devices, energy-providing solar panels, and other agencies. The movement of these parts generates various degrees of micro vibration [
1]. Despite not damaging the satellite structure, such micro vibration affects the pointing accuracy and stability of a space optical remote sensing satellite, obstructs the transfer of the photo-inducing charge and the motion synchronization of the focal plane image, and affects the quality of camera images [
2]. These effects restrict the developments in space optical remote sensing technology. Given that flywheel disturbance is the main source of micro vibration [
3], eliminating the effects of the flywheel rotary actuator disturbance on space cameras has become a key technology of high-precision stabilized platforms for spacecraft.