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.