Antenna combiner

• US 10,128,931 B2
• Filed: 07/17/2017
• Issued: 11/13/2018
• Est. Priority Date: 07/20/2016
• Status: Active Grant

• Current Assignee: Kymeta Corporation (Reorganized ISA SA)
• Original Assignee: Kymeta Corporation (Reorganized ISA SA)
• Inventors: Rothaar, Bruce, Preston, Shawn, Bialke, Nathan
• Primary Examiner(s): Nguyen, Duc M
• Application Number:
  US15/652,054
• Time in Patent Office: 484 Days
• CPC Class Codes: H01Q 13/103 with variable reactance for tuning the antenna tuning resonant circuits H03J
• CPC Class Codes: H01Q 21/0012 Radial guide fed arrays
• CPC Class Codes: H01Q 21/064 using horn or slot aerials slotted waveguides arrays H01Q21/005
• CPC Class Codes: H01Q 3/2605 Array of radiating elements provided with a feedback control over the element weights, e.g. adaptive arrays
• CPC Class Codes: H01Q 5/42 using two or more imbricated arrays H01Q5/49 takes precedence
• CPC Class Codes: H04B 7/0604 with predefined switching scheme
• CPC Class Codes: H04B 7/0608 Antenna selection according to transmission parameters
• CPC Class Codes: H04B 7/0814 based on current reception conditions, e.g. switching to different antenna when signal level is below threshold
• CPC Class Codes: H04B 7/084 Equal gain combining, only phase adjustments antenna beam scanning or forming by phase or amplitude control H01Q3/26, e.g. phased arrays
• CPC Class Codes: H04B 7/0857 using maximum ratio combining techniques, e.g. signal-to- interference ratio [SIR], received signal strenght indication [RSS]
• CPC Class Codes: H04B 7/0868 Hybrid systems, i.e. switching and combining
• CPC Class Codes: H04B 7/1851 Systems using a satellite or space-based relay H04B7/18508, H04B7/18521 take precedence; providing specific services H04B7/18523 - H04B7/18576

Abstract

An antenna combiner with transmission arbitration and method for using the same are described. In one embodiment, the apparatus comprises a plurality of antennas to receive signals from a satellite, each antenna in the plurality of antennas having a transmit aperture and a receive aperture, and wherein the receive aperture is operable to receive one of the signals from the satellite; a plurality of signal analyzers coupled to the plurality of antennas, each signal analyzer operable to determine signal quality of a distinct one antenna of the plurality of antennas; an arbiter coupled to the plurality of signal analyzers and operable to select one antenna of the plurality of antennas to transmit to the satellite based on results of determining the signal quality; and a first selector coupled to the arbiter and the plurality of antennas to cause data to be sent to the one antenna selected for transmission to the satellite.

Claims

1. An apparatus comprising:

a plurality of antennas, coupled to a moving platform, to receive signals from a satellite, each antenna in the plurality of antennas having a transmit aperture and a receive aperture, and wherein the receive aperture is operable to receive one of the signals from the satellite, wherein the plurality of antennas comprises a plurality of electronically-steerable flat panel antennas;

a plurality of signal analyzers coupled to the plurality of antennas, each signal analyzer operable to determine signal quality of a distinct one antenna of the plurality of antennas;

a prediction engine to generate predicted motion information indicative of a predicted location of each of the plurality of antennas for an expected time of satellite transmission based on motion information obtained from one or more sensors coupled to the plurality of antennas and expected transmission time;

an arbiter coupled to the plurality of signal analyzers and the prediction engine and operable to select one antenna of the plurality of antennas to transmit to the satellite based on results of determining the signal quality and the predicted location of each antenna of the plurality of antennas coupled to the moving platform;

a first selector coupled to the arbiter and the plurality of antennas to cause data to be sent to the one antenna selected for transmission to the satellite; and

a combiner coupled to the plurality of antennas to combine the signals received by the plurality of antennas into one signal, wherein the combiner is operable to coherently sum signals received by the plurality of antennas while the one antenna transmits to the satellite.

2. The apparatus defined in claim 1 wherein signals received by the plurality of antennas from the satellite are correlated.

3. The apparatus defined in claim 1 wherein the combiner is operable to combine the signals by coherently summing the signals using Maximal Ratio combining, equal gain combining, switched combining, or selection combining.

4. The apparatus defined in claim 1 further comprising:

a second selector operable to select a second antenna of the plurality of antenna to transmit data to the satellite in addition to the one antenna and send data to the satellite for transmission using the second antenna simultaneously with transmission to the satellite by the one antenna.

5. The apparatus defined in claim 1 wherein the first selector is operable to select the one antenna based on the one antenna having a higher signal quality than other antennas in the plurality of antennas.

6. The apparatus defined in claim 1 wherein the first selector is operable to determine antenna outages of each of the plurality of antennas based on the predicted motion and is operable to select the one antenna based on the determined antenna outages.

7. The apparatus defined in claim 1 wherein each of the plurality of electronically-steerable flat panel antennas having at least two spatially interleaved antenna arrays combined in a single physical aperture operable independently and simultaneously at distinct frequencies, wherein each of the at least two antenna sub-arrays comprises a tunable slotted array of antenna elements.

8. The apparatus defined in claim 1 wherein at least one of the transmit aperture and the receive aperture operates based on holographic beam forming.

9. The apparatus defined in claim 1 wherein the transmit aperture and the receive aperture of each antenna of the plurality of antennas comprises a tunable slotted array of antenna elements combined into a single physical aperture.

10. The apparatus defined in claim 9 wherein antenna elements of the transmit aperture and antenna elements of the receive aperture are interleaved and spaced with respect to each other.

11. The apparatus defined in claim 9 wherein each slotted array comprises a plurality of slots and further wherein each slot is tuned to provide a desired scattering at a given frequency.

12. The apparatus defined in claim 9 wherein each slotted array comprises:

a plurality of slots;

a plurality of patches, wherein each of the patches is co-located over and separated from a slot in the plurality of slots, forming a patch/slot pair, each patch/slot pair being turned off or on based on application of a voltage to the patch in the pair; and

a controller to apply a control pattern to control which patch/slot pairs are on and off to cause generation of a beam.

13. A method comprising:

receiving signals from a satellite using a plurality of antennas coupled to a moving platform, each antenna in the plurality of antennas having a transmit aperture and a receive aperture, wherein the plurality of antennas comprises a plurality of electronically-steerable flat panel antennas;

generating predicted motion information indicative of a predicted location of each of the plurality of antennas for an expected time of satellite transmission based on motion information obtained from one or more sensors coupled to the plurality of antennas and based on expected transmission time;

combining the signals received by the plurality of antennas into one signal using a combiner;

analyzing signal quality for each of the signals received by each of the plurality of antennas;

selecting one of the plurality of antennas to transmit to the satellite based on results of analyzing the signal quality and the predicted location of each antenna of the plurality of antennas coupled to the moving platform; and

transmitting data to the satellite using the one antenna while the combiner coherently sums signals received by the plurality of antennas.

14. The method defined in claim 13 wherein the signals from the satellite received by each antenna are correlated.

15. The method defined in claim 13 wherein combining the signals comprises coherently summing the signals using Maximal Ratio combining, equal gain combining, switched combining, or selection combining.

16. The method defined in claim 13 further comprising:

selecting a second antenna of the plurality of antenna to transmit data to the satellite in addition to the one antenna; and

transmitting data to the satellite using the second antenna simultaneously with transmission to the satellite by the one antenna.

17. The method defined in claim 13 wherein selecting the one antenna is based on the one antenna having a higher signal quality than other antennas in the plurality of antennas.

18. The method defined in claim 13 further comprising determining antenna outages of each of the plurality of antennas based on the predicted motion, and wherein selecting the one antenna is based on the determined antenna outages.

19. The method defined in claim 13 wherein each of the plurality of electronically-steerable flat panel antennas having at least two spatially interleaved antenna arrays combined in a single physical aperture operable independently and simultaneously at distinct frequencies, wherein each of the at least two antenna sub-arrays comprises a tunable slotted array of antenna elements.

20. The method defined in claim 13 wherein at least one of the transmit aperture and the receive aperture operates based on holographic beam forming.

21. An apparatus comprising:

a memory operable to store receive signal quality information for each of a plurality of antennas, wherein the plurality of antennas comprises a plurality of electronically-steerable flat panel antennas coupled to a moving platform;

a prediction engine to generate predicted motion information indicative of a predicted location of each of the plurality of antennas for an expected time of satellite transmission based on motion information obtained from one or more sensors coupled to the plurality of antennas and expected transmission time;

an arbiter coupled to the memory and the prediction engine and operable to select one antenna of the plurality of antennas to transmit to the satellite based on results of determining the signal quality and the predicted location of each antenna of the plurality of antennas coupled to the moving platform; and

a first selector coupled to the arbiter to cause data to be sent to the one antenna selected for transmission to the satellite; and

a combiner coupled to the plurality of antennas to combine the signals received by the plurality of antennas into one signal, wherein the combiner is operable to coherently sum signals received by the plurality of antennas while the one antenna transmits to the satellite.

22. The apparatus defined in claim 21 wherein the combiner is operable to combine the signals by coherently summing the signals using Maximal Ratio combining, equal gain combining, switched combining, or selection combining.

23. The apparatus defined in claim 21 wherein the first selector is operable to select the one antenna based on the one antenna having a higher signal quality than other antennas in the plurality of antennas.

24. The apparatus defined in claim 23 wherein the first selector is operable to select the one antenna of the plurality of antenna based on predicted motion of each antenna of the plurality of antennas.