Communications bandwidth enhancement using orthogonal spatial division multiplexing
View Patent ↗Systems and methods are described herein for communications bandwidth enhancement using Orthogonal Spatial Division Multiplexing (OSDM). For example, large sparse antenna arrays may be able to distinguish between signals emitted by multiple nearly collocated antennas, even if the signals have the same frequency, polarization, and coverage. Thus, the use of a large sparse antenna array may be able to resolve/isolate individual antennas on a single platform, allowing for OSDM, analogous to Orthogonal Frequency Divisional Multiplexing (OFDM). Using OSDM, multiple antennas on the same vehicle are able to reuse the same frequencies/polarizations without interference, thereby increasing spectrum availability while still providing the same transmitter power spectral density and total RF power emission.
1. A method for transmitting signals from multiple antennas from a communications platform, the method comprising:
receiving, at a first receiving station, a first combined signal comprising a first signal transmitted by a first antenna and a second signal transmitted by a second antenna, wherein:
the first signal and the second signal are transmitted at a single frequency, and
the first antenna and the second antenna are separated by a first distance;
receiving, at a second receiving station, a second combined signal comprising the first signal transmitted by the first antenna and the second signal transmitted by the second antenna, wherein:
the first receiving station and the second receiving station are separated by a second distance; and
determining the first signal and the second signal based on the received first combined signal and the received second combined signal;
wherein the second distance of separation between the first receiving station and the second receiving station is based on the first distance of separation between the first antenna and the second antenna such that an additive array factor is provided resulting in a peak on one of the first antenna and second antenna and a null on the other of the first antenna and second antenna, and wherein determining the first signal and the second signal is further based on the additive array factor.
2. The method of claim 1 wherein the first antenna and the second antenna are on a single satellite, aircraft, or other structure.
3. The method of claim 1 wherein the first antenna and the second antenna are on different satellites, aircraft, or other structures.
4. The method of claim 1 further comprising:
receiving, at a third receiving station, a third combined signal comprising the first signal transmitted by the first antenna and the second signal transmitted by the second antenna, wherein:
the third combined signal is different than the first combined signal and the second combined signal,
the third receiving station and the second receiving station are separated by a third distance.
5. The method of claim 4 , wherein the third distance is equal to the second distance.
6. The method of claim 1 , wherein the first combined signal and the second combined signal further comprise a third signal transmitted by a third antenna, wherein:
the first signal, the second signal, and the third signal are transmitted at the single frequency, and
the third antenna and the second antenna are separated by a third distance.
7. The method of claim 6 , wherein the third distance is equal to the first distance.
8. The method of claim 1 , wherein the second distance is larger than the first distance.
9. The method of claim 1 , wherein the first antenna and the second antenna are located at a geostationary earth orbit.
10. The method of claim 1 , wherein the first distance is a function of the satellite antenna spacing, satellite range, and signal wavelength.
11. A system for transmitting signals from multiple antennas, the system comprising:
a first receiving station configured to receive a first combined signal comprising a first signal transmitted by a first antenna and a second signal transmitted by a second antenna, wherein:
the first signal and the second signal are transmitted at a single frequency, and
the first antenna and the second antenna are separated by a first distance;
a second receiving station configured to receive a second combined signal comprising the first signal transmitted by the first antenna and the second signal transmitted by the second antenna, wherein:
the first receiving station and the second receiving station are separated by a second distance; and
processing circuitry configured to determine the first signal and the second signal based on the received first combined signal and the received second combined signa;
wherein the second distance of separation between the first receiving station and the second receiving station is based on the first distance of separation between the first antenna and the second antenna such that an additive array factor is provided resulting in a peak on one of the first antenna and second antenna and a null on the other of the first antenna and second antenna, and wherein determining the first signal and the second signal is further based on the additive array factor.
12. The system of claim 11 , wherein the first antenna and the second antenna are on a single satellite, aircraft, or other structure.
13. The system of claim 11 , wherein the first antenna and the second antenna are on different satellites, aircrafts, or other structures.
14. The system of claim 11 , further comprising a third receiving station configured to receive a third combined signal comprising the first signal transmitted by the first antenna and the second signal transmitted by the second antenna, wherein:
the third combined signal is different than the first combined signal and the second combined signal,
the third receiving station and the second receiving station are separated by a third distance.
15. The system of claim 14 , wherein the third distance is equal to the second distance.
16. The system of claim 11 , wherein the first combined signal and the second combined signal further comprise a third signal transmitted by a third antenna, wherein:
the first signal, the second signal, and the third signal are transmitted at the single frequency, and
the third antenna and the second antenna are separated by a third distance.
17. The system of claim 16 , wherein the third distance is equal to the first distance.
18. The system of claim 11 , wherein the second distance is larger than the first distance.
19. The system of claim 11 , wherein the first antenna and the second antenna are located at a geostationary earth orbit.
20. The system of claim 11 , wherein the first distance is a function of the satellite antenna spacing, satellite range, and signal wavelength.