Beam splitting hand off systems architecture
A beam splitting hand off systems architecture and method for using the same are disclosed. In one embodiment, the method comprises: generating a first beam with a single electronically steered flat-panel antenna to track a first satellite; generating a second beam with the single electronically steered flat-panel antenna to track a second satellite simultaneously while generating the first beam to track the first satellite; and handing off traffic from the first satellite to the second satellite.
1. An antenna for use in satellite communication, the antenna comprising:
an electronically steered flat-panel antenna aperture with a plurality of electronically controlled radio frequency (RF) radiating antenna elements; and
one or more processors configured to control the antenna aperture to
engage in full duplex communication with a first satellite, the full duplex communication using a first beam generated with the electronically steered flat-panel antenna aperture;
generate a split beam with the electronically steered flat-panel antenna aperture and point the split beam toward a second satellite to track the second satellite simultaneously while in full duplex communication with the first satellite; and
seamlessly hand off traffic from the first satellite to the second satellite to maintain connectivity throughout transition from the first satellite to the second satellite, including switching full duplex communications from between the electronically steered flat-panel antenna aperture and the first satellite to full duplex communications between the electronically steered flat-panel antenna aperture and the second satellite.
2. The antenna of claim 1 wherein the first and split beams are at different frequencies.
3. The antenna of claim 1 wherein the one or more processors are operable to generate pointing and tracking information with polarization values associated with each of the first and split beams and to communicate the pointing and tracking information with polarization values to the electronically steered flat-panel antenna aperture, wherein the pointing and tracking information comprises a pointing angle, frequency information, and symbol rate information.
4. The antenna of claim 3 further comprising an antenna control process module to send the pointing and tracking information to a pattern generation service, which generates first and second patterns to apply to first and second sets of radio-frequency (RF) radiating antenna elements, respectively, on the electronically steered flat-panel antenna aperture to generate the first and split beams, respectively, to point at carrier frequencies that differ in frequency, wherein the RF radiating antenna elements of the first and second sets are different.
5. The antenna of claim 4 wherein the first and second sets of RF radiating antenna elements have different numbers of RF radiating antenna elements.
6. The antenna of claim 4 wherein RF radiating antenna elements of the first and second sets of RF radiating antenna elements are arbitrarily distributed on the antenna aperture.
7. The antenna of claim 1 wherein the one or more processors are operable to turn off the first beam after handing off traffic from the first satellite to the second satellite.
8. The antenna of claim 1 wherein the one or more processors are operable to control the electronically steered flat-panel antenna aperture, prior to generating the split beam, to track the second satellite and generate the split beam to acquire a signal from the second satellite while generating the first beam.
9. The antenna of claim 1 wherein gain for the second beam is lower than gain for the first beam when using the split beam to acquire the signal from the second satellite.
10. The antenna of claim 1 wherein the split beam is wider than the first beam when using the second beam to acquire the signal from the second satellite.
11. The antenna of claim 1 wherein the one or more processors are operable to point the split beam to a predicted location of the second satellite, wherein the predicted location is based on commanded two-line elements (TLE).
12. A method for use with an antenna in a satellite communication system, the antenna having an electronically steered flat-panel antenna aperture with a plurality of electronically controlled radio frequency (RF) radiating antenna elements, the method comprising:
engaging, using in full duplex communication with a first satellite, the full duplex communication using a first beam generated with the electronically steered flat-panel antenna aperture;
generating a split beam with the electronically steered flat-panel antenna aperture to acquire a signal from a second satellite while generating the first beam while in full duplex communication between the first satellite and the electronically steered flat-panel antenna aperture;
pointing the split beam toward the second satellite to track the second satellite simultaneously while in full duplex communication with the first satellite; and
seamlessly hand off traffic from the first satellite to the second satellite to maintain connectivity throughout transition from the first satellite to the second satellite, including switching full duplex communications from between the electronically steered flat-panel antenna aperture and the first satellite to full duplex communications between the electronically steered flat-panel antenna aperture and the second satellite.
13. The method of claim 12 wherein the first and split beams are at different frequencies.
14. The method of claim 12 further comprising generating pointing and tracking information with polarization values associated with each of the first and split beams and providing the pointing and tracking information with polarization values to the electronically steered flat-panel antenna aperture, wherein the pointing and tracking information comprises a pointing angle, frequency information, and symbol rate information.
15. The method of claim 14 further comprising:
sending, by an antenna control process module, the pointing and tracking information to a pattern generation service; and
generating, by the pattern generation service, first and second patterns to apply to first and second sets of radio-frequency (RF) radiating antenna elements, respectively, on the electronically steered flat-panel antenna aperture to generate the first and split beams, respectively, to point at carrier frequencies that differ in frequency, wherein the RF radiating antenna elements of the first and second sets are different.
16. The method of claim 15 wherein the first and second sets of RF radiating antenna elements have different numbers of RF radiating antenna elements.
17. The method of claim 15 wherein RF radiating antenna elements of the first and second sets of RF radiating antenna elements are arbitrarily distributed on the antenna aperture.
18. The method of claim 12 further comprising turning off the first beam after handing off traffic from the first satellite to the second satellite.
19. The method of claim 12 wherein gain for the second beam is lower than gain for the first beam when using the split beam to acquire the signal from the second satellite.
20. The method of claim 12 wherein the split beam is wider than the first beam when using the second beam to acquire the signal from the second satellite.