Satellite ground terminal utilizing frequency-selective surface diplexer
Systems and methods are provided for separating the uplink signal from the downlink signal in a satellite communication system. A communication terminal for satellite communications is provided, comprising a reflector having a prime focus; a first feed located at the prime focus of the reflector and in optical communication with the reflector; a frequency-selective surface module having a reflected focus and located at a point along a communication path between the main reflector and the first feed; and a second feed located at the reflected focus of the frequency-selective surface module and in optical communication with the frequency-selective surface module.
1. A very small aperture terminal (VSAT) for a satellite communication system, comprising:
a reflector having a prime focus;
a first feed located at the prime focus of the reflector and in optical communication with the reflector;
a frequency-selective surface module having a reflected focus and located at a point along a communication path between the reflector and the first feed, wherein the frequency-selective surface module is configured to be transparent to a first set of frequencies such that a first signal within the first set of frequencies transmitted on a carrier signal passes through the frequency-selective surface module; and wherein the frequency-selective surface module is configured to be reflective to a second set of frequencies such that a second signal within the second set of frequencies transmitted on a carrier signal is reflected; and
a second feed located at the reflected focus of the frequency-selective surface module and in optical communication with the frequency-selective surface module, wherein each of the first and second feed is configured to transmit uplink signals within the first set of frequencies or receive downlink signals within the second set of frequencies,
wherein the frequency-selective surface module comprises a non-metallic base with a plurality of metallic traces embodied thereon, wherein the plurality of metallic traces are arranged in a pattern designed to allow a signal within the first set of frequencies to pass through the frequency-selective surface module, wherein the pattern comprises one or more of: strip gratings having a periodic array of conductive strips, mesh patterns, and cross-mesh patterns, and wherein the frequency-selective surface module comprises a horizontal adjustment support for adjusting a position of a surface of the frequency-selective surface module in a horizontal direction to ensure that the second feed is located at the reflected focus of the frequency-selective surface module.
2. The VSAT of claim 1 , wherein:
the first feed comprises a transmitter chain module and the second feed comprises a receiver chain module; or
the first feed comprises a receiver chain module and the second feed comprises a transmitter chain module.
3. The VSAT of claim 1 , wherein the non-metallic base comprises one or more of: resin, epoxy, plastic, phenolics, glass, fiberglass, silicon, gallium arsenide, silicon dioxide, sapphire, and aluminum oxide.
4. The VSAT of claim 1 , wherein the frequency-selective surface module is adjustable in one or more of a vertical direction and an angular direction, wherein the frequency-selective surface module comprises a notched support member such that the surface of the frequency-selective surface module may be raised or lowered to ensure that the surface is within the propagation path of the main reflector dish.
5. The VSAT of claim 1 , wherein each of the first feed and the second feed comprises a respective feed horn antenna.
6. A method of performing two-way satellite communication using a single antenna, comprising:
transmitting a carrier signal from a reflector of a very small aperture terminal (VSAT) to a frequency-selective surface module of the VSAT located within an optical path between the reflector and a prime focus of the reflector;
passing a first signal within a first frequency range through the frequency-selective surface module such that a first feed of the VSAT located at the prime focus of the reflector is in optical communication with the reflector; and
reflecting a second signal within a second frequency range at the frequency-selective surface module such that a second feed of the VSAT located at a reflected focus of the frequency-selective surface module is in optical communication with the reflector, wherein the frequency-selective surface module comprises a horizontal adjustment support for adjusting a position of a surface of the frequency-selective surface module in a horizontal direction to ensure that the second feed is located at the reflected focus of the frequency-selective surface module.
7. The method of claim 6 , wherein:
the first feed transmits uplink signals in a satellite communication system and the second feed receives downlink signals in a satellite communication system; or
the first feed receives downlink signals in a satellite communication system and the second feed transmits uplink signals in a satellite communication system.
8. The method of claim 6 , wherein each of the first feed and the second feed comprises a respective feed horn antenna.
9. The method of claim 6 , wherein the frequency-selective surface module has a parabolic shape.
10. The method of claim 6 , wherein the frequency-selective surface module comprises a non-metallic base with a plurality of metallic traces embodied thereon.
11. The method of claim 10 , wherein the plurality of metallic traces are arranged in a pattern designed to allow a signal within the first frequency range to pass through the frequency-selective surface module.
12. The method of claim 11 , wherein the pattern comprises one or more of: strip gratings having a periodic array of conductive strips, mesh patterns, and cross-mesh patterns.