A stabilization arrangement (10a-10d) for stabilizing an antenna mast, comprising • an antenna mast, and • a gyroscopic stabilizer device (12a, 12b), in turn comprising ∘ a flywheel, ∘ a flywheel axis, wherein the flywheel is rotatably arranged about the flywheel axis, and ∘ a gimbal structure (13a, 13b), wherein the flywheel and the flywheel axis are suspended in the gimbal structure (13a, 13b) and the gimbal structure (13a, 13b) is configured to permit flywheel precession about at least one gimbal output axis (16a, 16b), wherein the gyroscopic stabilizer device (12a, 12b) 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 (12a, 12b) is configured to reduce movements in a plane perpendicular to the extension of the antenna mast, wherein the at least one gimbal output axis (16a, 16b) is provided with a motor device connected to the gimbal output axis (16a, 16b), 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 (10a, 10d) 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 (12a, 12b), in turn comprising ∘ a flywheel, ∘ a flywheel axis, wherein the flywheel is rotatably arranged about the flywheel axis, and ∘ a gimbal structure (13a, 13b), wherein the flywheel and the flywheel axis are suspended in the gimbal structure (13a, 13b) and the gimbal structure (13a, 13b) is configured to permit flywheel precession about at least one gimbal output axis (16a, 16b), ∘ a flywheel, ∘ a flywheel axis, wherein the flywheel is rotatably arranged about the flywheel axis, and ∘ a gimbal structure (13a, 13b), wherein the flywheel and the flywheel axis are suspended in the gimbal structure (13a, 13b) and the gimbal structure (13a, 13b) is configured to permit flywheel precession about at least one gimbal output axis (16a, 16b), wherein the gyroscopic stabilizer device (12a, 12b) 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 (12a, 12b) is configured to reduce movements in a plane perpendicular to the extension of the antenna mast, wherein the at least one gimbal output axis (16a, 16b) is provided with a motor device connected to the gimbal output axis (16a, 16b), 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 (10a, 10d) 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.