A stabilization arrangement (10a-10d) for stabilizing an antenna mast , comprising • an antenna mast , and • a gyroscopic stabilizer device , in turn comprising ∘ a flywheel , ∘ a flywheel axis , wherein the flywheel is rotatably arranged about the flywheel axis , and ∘ a gimbal structure , wherein the flywheel and the flywheel axis are suspended in the gimbal structure and the gimbal structure is configured to permit flywheel precession about at least one gimbal output axis , wherein the gyroscopic stabilizer device is fixedly arranged in connection to a first end portion of the antenna mast and the antenna mast is fastenable to a supporting structure at a second end portion of the antenna mast , wherein the gyroscopic stabilizer device is configured to reduce movements in a plane perpendicular to the extension of the antenna mast , wherein the at least one gimbal output axis is provided with a motor device connected to the gimbal output axis , whereby by means of the motor device the precession about the gimbal output axis is actively controlled, wherein the antenna mast is provided with a rotating radar surface , characterized in that the stabilization arrangement is provided with a sensor in form of an anemometer , and wherein the motor device is configured to be controlled by taking into account: • the rate of rotation of the rotating radar surface , and • the wind speed measured by means of the anemometer . • an antenna mast , and • a gyroscopic stabilizer device , in turn comprising ∘ a flywheel , ∘ a flywheel axis , wherein the flywheel is rotatably arranged about the flywheel axis , and ∘ a gimbal structure , wherein the flywheel and the flywheel axis are suspended in the gimbal structure and the gimbal structure is configured to permit flywheel precession about at least one gimbal output axis , ∘ a flywheel , ∘ a flywheel axis , wherein the flywheel is rotatably arranged about the flywheel axis , and ∘ a gimbal structure , wherein the flywheel and the flywheel axis are suspended in the gimbal structure and the gimbal structure is configured to permit flywheel precession about at least one gimbal output axis , wherein the gyroscopic stabilizer device is fixedly arranged in connection to a first end portion of the antenna mast and the antenna mast is fastenable to a supporting structure at a second end portion of the antenna mast , wherein the gyroscopic stabilizer device is configured to reduce movements in a plane perpendicular to the extension of the antenna mast , wherein the at least one gimbal output axis is provided with a motor device connected to the gimbal output axis , whereby by means of the motor device the precession about the gimbal output axis is actively controlled, wherein the antenna mast is provided with a rotating radar surface , characterized in that the stabilization arrangement is provided with a sensor in form of an anemometer , and wherein the motor device is configured to be controlled by taking into account: • the rate of rotation of the rotating radar surface , and • the wind speed measured by means of the anemometer . • the rate of rotation of the rotating radar surface , and • the wind speed measured by means of the anemometer . <EOS>