Integrated commercial communications network using radio frequency and free space optical data communication

• US 9,166,684 B2
• Filed: 12/12/2014
• Issued: 10/20/2015
• Est. Priority Date: 05/31/2011
• Status: Active Grant

• Current Assignee: EOS Defense Systems USA Incorporated
• Original Assignee: Aoptix Technologies Incorporated
• Inventors: Pusarla, Chandrasekhar, Sivaprakasam, Srinivas, Shiran, Joseph, Northcott, Malcolm J., Graves, J. Elon, Dando, Howard, Basu, Santanu, Fleischer, Siegfried
• Primary Examiner(s): Sedighian, M. R.
• Assistant Examiner(s): Alagheband, Abbas H
• Application Number:
  US14/568,672
• Publication Number:
  US 20150098707A1
• Time in Patent Office: 312 Days
• Field of Search: 398/79, 398/115, 398118-131
• US Class Current: 1/1
• CPC Class Codes: H04B 10/112 Line-of-sight transmission over an extended range
• CPC Class Codes: H04B 10/1121 One-way transmission

Abstract

A stabilized ultra-high bandwidth capacity transceiver system that combines an E-band (71-76 GHz, 81-86 GHz) millimeter wave RF transceiver with an eye-safe adaptive optics Free Space Optical (FSO) transceiver as a combined apparatus for simultaneous point-to-point commercial communications. The apparatus has a high degree of assured carrier availability under stressing environmental conditions. The apparatus establishes and maintains pointing and stabilization of mmW RF and FSO optical beams between adjacent line of sight apparatuses. The apparatus can rapidly acquire and reacquire the FSO optical carrier link in the event the optical carrier link is impaired due to adverse weather.

Claims

1. An integrated apparatus for free space data transmission comprising:

an E-band millimeter wave (mmW) Radio Frequency (RF) transceiver comprising an RF antenna emitting an RF beam comprising a frequency of at least 71 GHz, the RF beam configured to locate a remote apparatus, assist in coarse control, and send data to the remote apparatus, the RF antenna configured to receive a received RF beam from the remote apparatus;

a free space optical (FSO) transceiver comprising an optical source emitting an optical beam through a FSO telescope configured to assist in fine orientation control and send data to the remote apparatus, the FSO telescope configured to receive a received optical beam from the remote apparatus, the optical beam pointed in substantially the same direction as the RF beam, the RF antenna and the FSO telescope having physically separate transmission axes located a distance greater than zero centimeters apart;

at least one steering assembly that steers the RF beam and the FSO beam towards the remote apparatus;

a controller configured to perform coarse orientation control of the steering assembly based on the received RF beam, and to perform fine orientation control of the steering assembly based on the received optical beam.

2. The integrated apparatus of claim 1 wherein the at least one steering assembly comprises a common moving platform connected to both the RF transceiver and the FSO transceiver, the common moving platform causing the RF beam and the FSO beam to both be commonly steered towards the remote apparatus.

3. The integrated apparatus of claim 1

wherein the at least one steering assembly comprises a first steering assembly for the RF transceiver, and a second steering assembly for the FSO transceiver, the first and second steering assemblies being independently steerable from each other;

and

wherein to steer the RF beam and the FSO beam towards the remote apparatus the first and second steering assemblies are both separately steered to orient the RF beam and the FSO beam at a same angle.

4. The integrated apparatus of claim 1 wherein the RF beam provides control information for a transmit intensity of an optical signal transmitted by the remote apparatus, the control information based on an intensity of the received optical beam.

5. The integrated apparatus of claim 1 wherein the optical beam transmitted by the FSO transceiver is substantially collimated.

6. The integrated apparatus of claim 1 wherein the FSO transceiver comprises an adaptive optics system to partially correct received and transmitted optical wavefronts.

7. The integrated apparatus of claim 6 wherein the adaptive optics comprises a wavefront sensor to measure wavefront error, including tip-tilt.

8. The integrated apparatus of claim 1 wherein the FSO transceiver transmits data over a plurality of channels using dense wavelength division multiplexing (DWDM).

9. The integrated apparatus of claim 1 wherein both the RF transceiver and the FSO transceiver are capable of operating at a plurality of data carrier rates.

10. The integrated apparatus of claim 1 comprising a movable platform coupling the mmW RF transceiver and the FSO transceiver, and wherein the at least one steering assembly is a gimbal assembly.

11. The integrated apparatus of claim 1 comprising an environmental enclosure including the mmW RF transceiver, the FSO transceiver, the steering assembly, and an aperture aligned with the FSO transceiver to permit data transmission.

12. The integrated apparatus of claim 11 wherein the aperture of the environmental enclosure comprises an optical window transparent to the transmissions of the FSO transceiver and a heater to prevent condensation on the optical window.

13. The integrated apparatus of claim 1

wherein the integrated apparatus is installed at a first cell site or a network point of presence;

and

wherein the remote apparatus is installed at a second cell site or a network point of presence that is physically remote from the first cell site.

14. A method for maintaining a communications link with a remote apparatus comprising:

transmitting a radio frequency (RF) beam from an RF antenna of an E-band millimeter wave (mmW) (RF) transceiver, the RF beam comprising a frequency of at least 71 GHz;

receiving an E-band RF response beam at the RF antenna;

adjusting an orientation of at least one steering assembly based on the E-band RF response beam, the at least one steering assembly steering the E-band mmW RF transceiver and a Free Space Optical (FSO) transceiver towards the remote apparatus;

transmitting a free space optical (FSO) beam from a FSO telescope of the FSO transceiver, the RF antenna and the FSO telescope having physically separate transmission axes located a distance greater than zero centimeters apart

receiving an FSO response beam at the FSO telescope; and

adjusting the orientation of the at least one steering assembly based on the FSO response beam.

15. The method of claim 14 wherein the at least one steering assembly comprises a common moving platform connected to both the RF transceiver and the FSO transceiver, the common moving platform causing the RF transceiver and the FSO transceiver to both be steered towards the remote apparatus.

16. The method of claim 14 wherein the at least one steering assembly comprises a first steering assembly for the RF transceiver, and a second steering assembly for the FSO transceiver, the first and second steering assemblies being independently steerable from each other;

and

wherein to steer the RF antenna and the FSO telescope towards the remote apparatus the first and second steering assemblies are both steered a same direction.

17. The method of claim 14, wherein adjusting the orientation of the at least one steering assembly based on the FSO response signal comprises applying a centroid algorithm to the FSO response signal.

18. The method of claim 14, wherein adjusting the orientation of the steering assembly based on the FSO response signal comprises:

measuring a wavefront of the FSO response signal using a wavefront sensor, the wavefront comprising a tip-tilt component;

controlling a fast steering mirror (FSM) and the at least one steering assembly using the tip-tilt component of the wavefront.

19. The method of claim 18, further comprising controlling a deformable mirror using the wavefront.