A momentum-wheel installed to provide attitude-control torque actually producesundesirable force or torque disturbances owing to wheel imbalance and imperfection of theball-bearings. To improve the pointing performance of observation satellites, a vibrationisolator is used to isolate observation devices from these disturbances. This paper comparesthree types of semi-active isolators that consist of a piezoelectric material and aswitch-controlled passive circuit. Since this isolation is implemented by controlling a circuitswitch no external energy is supplied to the system, and so the system is stable even whena malfunction occurs in control. We propose a simple but effective isolation method thatneeds to know only one velocity value instead of the full state of the system. Numericalsimulations with a simple model of an observation satellite demonstrated that the proposedisolator works well to isolate an observation device from disturbances caused by themomentum-wheel, without causing any degradation in the attitude control of satellites.