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. A method for use in satellite communication, the method comprising:
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 acquire a second satellite simultaneously while generating the first beam to track the first satellite, wherein the first and second beams have different antenna gains when the second beam is to acquire the second satellite and the first beam is to track the first satellite;
generating the second beam with the single electronically steered flat-panel antenna to track the second satellite simultaneously while generating the first beam to track the first satellite, direction of the first and second beams being electronically controlled by the single electronically steered flat-panel antenna that electronically scans in multiple dimensions; and
handing off traffic from the first satellite to the second satellite.
2. The method of claim 1 wherein gain for the second beam is lower than gain for the first beam when the second beam is used for acquiring the signal from the second satellite.
3. The method of claim 1 wherein the second beam is wider than the first beam when used for acquiring the signal from the second satellite.
4. The method of claim 1 wherein handing off traffic is performed seamlessly such that connectivity is maintained throughout the transition from the first satellite to the second satellite.
5. The method of claim 1 further comprising generating first and second patterns to apply to first and second sets of radio-frequency (RF) radiating antenna elements, respectively, on an antenna aperture of the electronically steered flat-panel antenna to generate the first and second 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.
6. The method of claim 5 wherein the first and second sets of RF radiating antenna elements have a different number of RF radiating antenna elements.
7. The method of claim 5 wherein RF radiating antenna elements of the first and second sets of RF radiating antenna elements are arbitrarily distributed on the antenna aperture.
8. The method of claim 1 wherein the second beam is pointed to a predicted location of the second satellite.
9. The method of claim 8 wherein the predicted location is based on commanded two-line elements (TLE).
10. The method of claim 1 further comprising:
prior to generating the first beam to track the first satellite,
operating the electronically steered flat-panel antenna in a single-beam configuration in which the electronically steered flat-panel antenna is generating a single beam, including generating a third beam to track the second satellite using a first set of RF radiating antenna elements on an antenna aperture of the electronically steered flat-panel antenna, the first set of RF radiating antenna elements including RF radiating elements of a second set of RF radiating elements on the antenna aperture for generating the first beam and RF radiating elements of a third set of RF radiating elements on the antenna aperture for generating the second beam; and
determining to switch the electronically steered flat-panel antenna to a two-beam configuration in which the electronically steered flat-panel antenna is generating the first and second beams.
11. The method of claim 10 wherein the first set of RF radiating antenna elements includes the second and third set of RF radiating elements.
12. 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 coupled to the antenna aperture to control the antenna aperture to generate a first beam with a single electronically steered flat-panel antenna to track a first satellite; generate a second beam with the single electronically steered flat-panel antenna to acquire a second satellite simultaneously while generating the first beam to track the first satellite, wherein the first and second beams have different antenna gains when the second beam is to acquire the second satellite and the first beam is to track the first satellite; generate the second beam with the single electronically steered flat-panel antenna to track the second satellite simultaneously while generating the first beam to track the first satellite, where direction of the first and second beams is being electronically controlled by the single electronically steered flat-panel antenna that electronically scans in multiple dimensions; and hand off traffic from the first satellite to the second satellite.
13. The antenna of claim 12 wherein gain for the second beam is lower than gain for the first beam when the second beam is used for acquiring the signal from the second satellite.
14. The antenna of claim 12 wherein the second beam is wider than the first beam when used for acquiring the signal from the second satellite.
15. The antenna of claim 12 wherein handing off traffic is performed seamlessly such that connectivity is maintained throughout the transition from the first satellite to the second satellite.
16. The antenna of claim 12 further comprising generating first and second patterns to apply to first and second sets of radio-frequency (RF) radiating antenna elements, respectively, on an antenna aperture of the electronically steered flat-panel antenna to generate the first and second 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.
17. The antenna of claim 16 wherein the first and second sets of RF radiating antenna elements have a different number of RF radiating antenna elements.
18. The antenna of claim 16 wherein RF radiating antenna elements of the first and second sets of RF radiating antenna elements are arbitrarily distributed on the antenna aperture.
19. The antenna of claim 12 wherein the second beam is pointed to a predicted location of the second satellite, wherein the predicted location is based on commanded two-line elements (TLE).
20. The antenna of claim 12 further comprising:
prior to generating the first beam to track the first satellite,
operating the electronically steered flat-panel antenna in a single-beam configuration in which the electronically steered flat-panel antenna is generating a single beam, including generating a third beam to track the second satellite using a first set of RF radiating antenna elements on an antenna aperture of the electronically steered flat-panel antenna, the first set of RF radiating antenna elements including RF radiating elements of a second set of RF radiating elements on the antenna aperture for generating the first beam and RF radiating elements of a third set of RF radiating elements on the antenna aperture for generating the second beam; and
determining to switch the electronically steered flat-panel antenna to a two-beam configuration in which the electronically steered flat-panel antenna is generating the first and second beams.
21. A method for use in satellite communication, the method comprising:
engaging in full duplex communication with a first satellite, the full duplex communication using a first beam generated with a single electronically steered flat-panel antenna;
generating a split beam with the single electronically steered flat-panel antenna and pointing the split beam toward a second satellite track the second satellite simultaneously while in full duplex communication with the first satellite with the single electronically steered flat-panel antenna, direction of the first and split beams being electronically controlled in two-dimensions using the single electronically steered flat-panel antenna; and
seamlessly handing 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 single electronically steered flat-panel antenna and the first satellite to full duplex communications between the single electronically steered flat-panel antenna and the second satellite.
22. The method of claim 21 further comprising turning off the first beam after handing off traffic from the first satellite to the second satellite.
23. The method of claim 21 further comprising:
prior to generating the split beam to track the second satellite, generating the split beam to acquire a signal from the second satellite while generating the first beam.
24. The method of claim 21 further comprising generating first and second patterns to apply to first and second sets of radio-frequency (RF) radiating antenna elements, respectively, on an antenna aperture of the electronically steered flat-panel antenna 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.