Antenna system for satellite communication
View Patent ↗An antenna system for satellite communication, mounted on a moving platform, includes an antenna assembly, a control and display unit, and an antenna steering unit. The antenna assembly includes mounted on an antenna mast. The antenna steering unit includes a support housing, a rotary joint comprising a BNC connector, an electronic magnetic compass. an angular velocity-sensing gyroscope, a global positioning system receiver, a signal processor and a motor. The direction of the antenna's azimuth axis is determined based on the heading of the moving platform determined by the signal processor. In one embodiment, the director elements, the antenna mast and the azimuth mast are all articulated on flexible joints comprising a cable and spring mechanism allowing the director elements to fold toward the antenna mast and allowing the antenna assembly to fold toward the azimuth mast for stowing.
1. An antenna system for satellite communication mounted on a moving platform, comprising:
an antenna assembly, comprising:
an eggbeater antenna mounted on an antenna mast;
a control and display unit;
an antenna steering unit, comprising:
a support housing;
a rotary joint comprising a BNC connector, wherein the BNC connector has a first part connected to the support housing of the antenna steering unit, and a second part connected to the antenna assembly at the axis of rotation, such that when the antenna rotates, the BNC connector rotates in synchronism with it;
an electronic magnetic compass for sensing the Earth magnetic field to determine a reference azimuth;
an angular velocity-sensing gyroscope for sensing motion and outputting an angular velocity output signal;
a global positioning system receiver for providing track of the moving platform;
a signal processor in communication with the electronic magnetic compass, the angular velocity-sensing gyroscope and the global positioning system receiver for receiving the reference azimuth, the angular velocity output signal, and the track, and determining the heading of the moving platform using an adaptive time interval; and
a motor that controls direction of the antenna's azimuth axis, wherein the direction of the antenna's azimuth axis is determined based on the heading of the moving platform determined by the signal processor.
2. The antenna system of claim 1 , wherein the eggbeater antenna comprises a pair of crossed curved elements forming loops and a ring reflector torus.
3. The antenna system of claim 2 , wherein the ring reflector torus comprises metal.
4. The antenna system of claim 2 , wherein the ring reflector comprises a conductive material.
5. The antenna system of claim 2 , wherein a diameter of the ring reflector torus measures between about 12″ to about 18″.
6. The antenna system of claim 2 , wherein a cross-sectional diameter of the ring reflector torus measures between about 0.5″ to about 1.5″.
7. The antenna system of claim 2 , wherein a diameter of the ring reflector torus measures about 15″.
8. The antenna system of claim 2 , wherein a cross-sectional diameter of the ring reflector torus measures about 1″.
9. An antenna system for satellite communication mounted on a moving platform, comprising:
an antenna assembly, comprising:
a pair of crossed curved elements forming loops, and a conductive ring reflector torus;
a control and display unit;
an antenna steering unit, comprising:
a support housing;
a rotary joint comprising a BNC connector, wherein the BNC connector has a first part connected to the support housing of the antenna steering unit, and a second part connected to the antenna assembly at the axis of rotation, such that when the antenna rotates, the BNC connector rotates in synchronism with it;
an electronic magnetic compass for sensing the Earth magnetic field to determine a reference azimuth;
an angular velocity-sensing gyroscope for sensing motion and outputting an angular velocity output signal;
a global positioning system receiver for providing track of the moving platform;
a signal processor in communication with the electronic magnetic compass, the angular velocity-sensing gyroscope and the global positioning system receiver for receiving the reference azimuth, the angular velocity output signal, and the track, and determining the heading of the moving platform using an adaptive time interval; and
a motor that controls direction of the antenna's azimuth axis, wherein the direction of the antenna's azimuth axis is determined based on the heading of the moving platform determined by the signal processor.
10. The antenna system of claim 9 , wherein the conductive ring reflector torus comprises metal.
11. The antenna system of claim 9 , wherein a diameter of the conductive ring reflector torus measures between about 12″ to about 18″.
12. The antenna system of claim 9 , wherein a cross-sectional diameter of the conductive ring reflector torus measures between about 0.5″ to about 1.5″.
13. The antenna system of claim 9 , wherein a diameter of the conductive ring reflector torus measures about 15″.
14. The antenna system of claim 9 , wherein a cross-sectional diameter of the conductive ring reflector torus measures about 1″.