Payload for a multibeam communication satellite of a hub-spoke system with receive and transmit switching pattern synchronized over a frame for flexible forward and return capacity allocation
US-2015009891-A1 · Jan 8, 2015 · US
US9401759B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9401759-B2 |
| Application number | US-201414510790-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 9, 2014 |
| Priority date | Oct 9, 2014 |
| Publication date | Jul 26, 2016 |
| Grant date | Jul 26, 2016 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
Multibeam coverage for a high altitude platform is disclosed. An example apparatus includes a plurality of antennas configured to provide communication coverage among a plurality of terminals within a specified area on the ground, each antenna being configured to communicate with a specified cell within the specified area. The antennas of the example apparatus have differently sized apertures to maintain a similar surface spectral density among the cells within the specified area.
Opening claim text (preview).
The invention is claimed as follows: 1. A telecommunications platform apparatus comprising: a plurality of antennas configured to provide communication coverage among a plurality of terminals within a specified area on the ground, each antenna being configured to communicate with a specified cell within the specified area, wherein the antennas have differently sized apertures to maintain a similar surface spectral density among the cells within the specified area. 2. The apparatus of claim 1 , wherein the plurality of terminals includes user terminals and a gateway, and wherein communications are between the gateway and the user terminals. 3. The apparatus of claim 2 , wherein each of the antennas that communicates with the gateway is at least one of mechanically and electrically controlled to continually point at the gateway. 4. The apparatus of claim 1 , wherein the plurality of terminals associated with the telecommunications platform communicates with a plurality of terminals associated with a second telecommunications platform via a communications link between the telecommunications platforms. 5. The apparatus of claim 1 , wherein the apertures of the antennas corresponding to cells at outer edges of the specified area have a larger area than apertures of antennas corresponding to cells within a center of the specified area. 6. The apparatus of claim 1 , wherein the telecommunications platform apparatus includes a low earth orbit satellite. 7. The apparatus of claim 1 , wherein the telecommunications platform apparatus includes a high altitude platform. 8. The apparatus of claim 7 , wherein the high altitude platform operates between 17 km and 22 km above a center of the specified area of the ground. 9. The apparatus of claim 1 , wherein the plurality of antennas is configured to provide substantially uniform spectral density coverage to each of the plurality of terminals. 10. The apparatus of claim 1 , wherein the telecommunications platform apparatus is communicatively coupled to a GEO satellite. 11. The apparatus of claim 1 , wherein the telecommunications platform apparatus causes the cells on the surface to remain substantially stationary. 12. The apparatus of claim 1 , wherein the telecommunications platform apparatus causes the cells on the surface to move within the specified area. 13. The apparatus of claim 1 , wherein each of the cells has an approximately hexagonal-shape and the antennas are arranged such that the corresponding cells form a honeycomb shape within the specified area. 14. The apparatus of claim 13 , wherein the apertures of the antennas are configured such that each of the hexagonal-shaped cells has a similar area. 15. The apparatus of claim 1 , wherein the plurality of antennas includes 19 antennas and the specified area is partitioned into 19 cells such that: the 19 cells have an area of 878 km 2 and a radius of 16.7 km; an antenna corresponding to a cell within a center of the specified area is configured to have a beamwidth of 79.7° and an aperture diameter of 0.35 inches conditioned on the apparatus operating between 28 to 30 GHz; six antennas corresponding to six cells around the center cell of the specified area are configured to have an elliptical 3 dB beam contour of 25.6° by 52°, an aperture with dimensions of 1.07 by 0.47 inches, and a gain of 13.4 dB conditioned on the apparatus operating between 28 to 30 GHz; and 12 antennas corresponding to 12 cells around the six cells of the specified area are configured to have an elliptical 3 dB beam contour of 8.9° by 28°, an aperture with dimensions of 3.11 by 1.0 inches, and a gain of 21 dB conditioned on the apparatus operating between 28 to 30 GHz. 16. The apparatus of claim 15 , wherein the antennas each have a downlink spectrum of 150 MHz. 17. The apparatus of claim 15 , wherein the center antenna includes an open ended waveguide antenna, the six antennas include small horn antennas, and the 12 antennas include small reflector antennas. 18. The apparatus of claim 15 , wherein the antennas are at least one of fixed or variable phased array antennas. 19. The apparatus of claim 1 , wherein the plurality of antennas includes 25 antennas and the specified area is partitioned into 25 cells such that: an inner seven cells have an area of 125 km 2 and a radius of 6.3 km; an antenna corresponding to a central cell of the inner seven cells within a central area of the specified area is configured to have a beamwidth of 35.1°, an aperture diameter of 0.78 inches, and a gain of 14.1 dB conditioned on the apparatus operating between 28 to 30 GHz; six antennas corresponding to six cells of the inner seven cells positioned around the center cell of the specified area are configured to have an elliptical 3 dB beam contour of 22.3° by 33°, an aperture with dimensions of 1.23 by 0.83 inches, and a gain of 16.3 dB conditioned on the apparatus operating between 28 to 30 GHz; six antennas corresponding to outer six cells around the seven inner cells of the specified area are configured to have an elliptical 3 dB beam contour of 25.6° by 52°, an aperture with dimensions of 1.07 by 0.47 inches, and a gain of 13.4 dB conditioned on the apparatus operating between 28 to 30 GHz; and 12 antennas corresponding to 12 cells around the outer six cells of the specified area are configured to have an elliptical 3 dB beam contour of 8.9° by 28°, an aperture with dimensions of 3.11 by 1.0 inches, and a gain of 21 dB conditioned on the apparatus operating between 28 to 30 GHz. 20. The apparatus of claim 19 , wherein the seven antennas corresponding to the seven inner cells are configured to cover the cells each with an area of about 125 km 2 , the six antennas are configured to cover the six outer cells each with an area of about 878 km 2 , and the 12 antennas are configured to cover cells each with an area of about 878 km 2 . 21. The apparatus of claim 19 , wherein the seven antennas, corresponding to the seven inner cells, each have a spectrum of 21.4 MHz, the six antennas, corresponding to the six outer cells, each have a spectrum of 150 MHz, and the 12 antennas each have a spectrum of 150 MHz. 22. The apparatus of claim 1 , wherein the plurality of antennas includes 37 antennas and the specified area is partitioned into 37 cells such that: each cell has an area of 450 km 2 and a radius of 12 km; one antenna corresponding to a central cell within the specified area is configured to have a beamwidth of 61.8°, an aperture diameter of 0.45 inches, and a gain of 9.2 dB conditioned on the apparatus operating between 28 to 30 GHz; six antennas corresponding to six cells around the central cell of the coverage area are configured to have an elliptical 3 dB beam contour of 26.7° by 47°, an aperture with dimensions of 1.03 by 0.59 inches, and a gain of 14 dB conditioned on the apparatus operating between 28 to 30 GHz; 12 antennas corresponding to 12 cells around the six cells of the coverage area are configured to have an elliptical 3 dB beam contour of 8.9° by 28°, an aperture with dimensions of 2.46 by 1.02 inches, and a gain of 20.2 dB conditioned on the apparatus operating between 28 to 30 GHz; and 19 antennas corresponding to 19 cells around the 12 cells of the coverage are configured to have an elliptical 3 dB beam contour of 5.5° by 18°, an aperture with dimensions of 5.0 by 1.5 inches, and a gain of 25 dB conditioned on the apparatus operating between 28 to 30 GHz. 23. The apparatus of cl
Transmission in a satellite or space-based system · CPC title
Systems using a satellite or space-based relay (H04B7/18508, H04B7/18521 take precedence; providing specific services H04B7/18523 - H04B7/18576) · CPC title
Space-based or airborne stations; {Stations for satellite systems}(H04B7/204 takes precedence) · CPC title
Spot beam multiple access · CPC title
for geolocalisation of a station (position fixing by direction or distance determination G01S5/00) · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.