The invention discloses a test 
system for simulating flexible 
satellite three-axis attitude 
coupling movement with a single-axis 
air bearing table. The single-axis 
air bearing table is adopted for simulating the attitude movement of one axis of the 
satellite. The 
system comprises an attitude track 
control unit, an 
inertia reference unit, a mathematic model resolving unit, a control execution mechanism, an angle measuring device and a force moment 
output device, wherein the 
inertia reference unit is connected with the attitude track 
control unit, the mathematic model resolving unit is connected with the attitude track 
control unit, the control execution mechanism is connected with the attitude track control unit and the 
inertia reference unit, the angle measuring device is connected with the attitude track control unit, and the force moment 
output device is connected with the attitude track control unit. According to the test 
system for simulating flexible 
satellite three-axis attitude 
coupling movement, function extension is carried out on the single-axis 
air bearing table, the 
physical property and a mathematic model are combined, and resolving is carried out through the mathematic model, so that three-axis 
coupling force moment, flexible attachment disturbance force moment and 
space environment disturbance force moment borne by the satellite in the single-axis attitude movement process are achieved through a force moment 
output device, the effectiveness for verifying the flexible satellite single-axis attitude movement with the single-axis air bearing table can be improved, and the satellite ontrack single-axis attitude movement can be reflected more really.