Processing of multiple wavelength signals transmitted through free space

• US 7,072,591 B1
• Filed: 01/21/2002
• Issued: 07/04/2006
• Est. Priority Date: 06/23/1999
• Status: Expired due to Term

• Current Assignee: BAE Systems Space & Mission Systems Incorporated (BAE Systems Plc)
• Original Assignee: Ball Aerospace & Technologies Corporation (Ball Corporation)
• Inventors: Smith, Robert J.
• Primary Examiner(s): Bello, Agustin
• Application Number:
  US10/054,150
• Time in Patent Office: 1,625 Days
• Field of Search: 398118-131, 398182-201, 398202-214
• US Class Current: 398/202
• CPC Class Codes: H04B 10/1121 One-way transmission

Abstract

The present invention is directed to a laser communication receiver for wireless optical communication. A laser communication receiver includes a diffractive optical element to permit detectors at different spatial locations to detect different wavelengths of the optical signal. An immersion lens may be employed to focus the optical signal to a spot size smaller than the photoactive area of the detector. In one detector configuration, the optical signal is folded by a reflective surface and focused on a plurality of stacked detectors. The present invention further provides a method of manufacturing a detector and immersion lens assembly that provides a high degree of alignment between the lens and the corresponding detector.

Claims

1. A method for receiving high frequency signals, comprising:

transmitting a coherent beam comprising at least one signal including first and second data modulated onto the beam from a laser transmitter through atmospheric turbulence to a receiver, wherein a diameter of the beam comprising said at least one signal is less than an inner scale of an atmosphere at an aperture of said transmitter, wherein a divergence angle of the beam is selected so that it exceeds a determined turbulence induced beam deviation so that a far-field footprint of the beam remains on the receiver aperture despite the atmospheric turbulence, wherein the receiver is located at a distance from the transmitter, wherein the at least one signal, after transmission through the atmospheric turbulence, has a distorted wave-front, wherein said transmitting of said first and second data is conducted at a rate greater than one gigabit/second, and wherein each of said first and second data is associated with first and second wavelength channels, respectively, the first wavelength channel being different from the second wavelength channel;

receiving said at least one distorted signal including said first and second data at a detector assembly associated with said receiver;

detecting said first data using a first detector unit of the detector assembly, wherein the first detector unit is located at a first position; and

detecting said second data using a second detector unit of the detector assembly, wherein the second detector unit is located at a second position that is different from said first position.

2. A method, as claimed in claim 1, wherein:

said detecting first data step includes detecting at the same time, using said first detector unit, all of said first data that was received by said first position of said detector assembly at a particular instance in time.

3. A method, as claimed in claim 1, wherein:

said detecting first data step includes accepting a focal spot size diameter of greater than 40 microns and then reducing said focal spot size diameter.

4. A method, as claimed in claim 3, wherein:

said reducing step includes using a focusing element having a refractive index greater than 2.

5. A method, as claimed in claim 4, wherein:

said focusing element has a traverse length along and through which said first data having said associated first wavelength channel passes, and the speed of said first data in passing along and through said traverse length is no greater than 30% of the speed of light in air.

6. A method, as claimed in claim 3, wherein:

said focal spot size diameter is greater than about 100 microns.

7. A method, as claimed in claim 1, wherein:

said detector assembly includes a linking device, a focusing element and a detector unit.

8. A method, as claimed in claim 1, further comprising after the transmitting step:

finitely focusing, with a holographic unit, said first data to form a first beam and second data to form a second beam.

9. A method, as claimed in claim 1, wherein:

said detecting first data step includes reflecting said first data associated with said first wavelength channel by a first mirror to a focusing element and with an output of said focusing element being in communication with said first detector unit.

10. A method, as claimed in claim 1, wherein in said receiving step said first data is finitely focused on a first focal point and said second data is finitely focused on a second focal point and the first points is at least substantially at the first location and the second focal point is at least substantially at the second location.

11. A method, as claimed in claim 1, wherein:

said detecting said second data step includes accepting said second data using a linking device, directing said second data to a second focusing element and with the output of said second focusing element being in communication with said second detector unit.

12. A method, as claimed in claim 1, wherein said transmitting step includes:

modulating said first and second data on a respective light beam to form first and second modulated light beams, respectively, and further comprising;

demodulating the detected first and second data.

13. A method, as claimed in claim 7, wherein a first linking device corresponds to the first detector and a second linking device corresponds to the second detector, wherein the first and second linking devices are in different spatial locations, wherein the first data detecting step comprises:

redirecting, with the first linking device, said first data from a first optical path to a transversely oriented second optical path, the second optical path intersecting the first detector unit; and

wherein said second data detecting step comprises;

redirecting, with the second linking device, said second data from a third optical path to a transversely oriented fourth optical path, the fourth optical path intersecting the second detector unit.

14. A method, as claimed in claim 1, wherein a spacing between said first and second wavelength channels is about 4 nanometers.

15. A system for receiving high frequency signals, comprising:

a receiver that receives at least one signal including first and second data and comprises a detector assembly; and

a transmitter that transmits the at least one signal as a beam having a diameter that is less than an inner scale of an atmosphere at or near a transmitter aperture through atmospheric turbulence to the receiver, wherein the receiver is located at a distance of greater than 100 m from the transmitter, wherein the atmospheric turbulence is determined to be associated with a worst case atmospheric turbulence induced deviation of the beam, wherein a divergence angle of the beam is selected to exceed the atmospheric turbulence induced beam deviation for the beam under the determined worst case conditions, wherein the at least one signal, after transmission through the atmospheric turbulence, has a distorted wavefront, wherein said first and second data are each transmitted at a rate greater than one gigabit/second, wherein said first and second data are respectively associated with first and second wavelength channels, the first wavelength channel being different from the second wavelength channel, and wherein the detector assembly comprises at least a first detector unit located at a first position for detecting said first data, and a second detector unit located at a second position for detecting the second data, the second position being different from said first position.

16. A system, as claimed in claim 15, wherein:

said detector assembly includes a first focusing element that finitely focuses the first data onto the first detector unit, wherein a focal spot size of the first data has a diameter of greater than 40 microns.

17. A system, as claimed in claim 16, wherein:

said focusing element has a refractive index greater than 2.

18. A system, as claimed in claim 17, wherein:

said focusing element has a traverse length along and through which said first data having said associated first wavelength channel passes, and the speed of said first data in passing along and through said traverse length is no greater than 30% of the speed of light in air.

19. A system, as claimed in claim 17, wherein:

said focal spot size diameter is greater than about 100 microns.

20. A system, as claimed in claim 15, wherein:

said detector assembly includes a linking device, a focusing element and a detector unit.

21. A system, as claimed in claim 15, further comprising:

a holographic unit that finitely focuses said first and second data in said at least one distorted signal at the first and second locations.

22. A system, as claimed in claim 16, wherein the detector assembly comprises:

a first mirror that reflects said first data associated with said first wavelength channel onto the focusing element.

23. A method for receiving high frequency data associated with at least a first wavelength channel, comprising:

receiving at a first receiving location said first wavelength channel after the first wavelength channel has passed through atmospheric turbulence and thereby become optically distorted;

finitely focusing said received first wavelength channel with a first optical element to form a focused first beam having a focused first spot size, wherein said first focused beam is focused at a first location;

further finitely focusing the focused first beam with a second optical element at said first location to form a further focused first beam having a further focused first spot size that is smaller than the focused first spot size, wherein the first and second optical elements are at different spatial locations;

detecting at least a portion of the data in the further focused first beam;

receiving at said first receiving location a second wave length channel after the second wave length channel has passed through atmospheric turbulence and thereby become optically distorted, wherein said first and second wavelength channels are transmitted as part of a first beam;

finitely focusing said received second wavelength channel with said first optical element to form a focused second beam having a focused second spot size, wherein said second focus beam is focused at a second location;

further finitely focusing the focused second beam with a third optical element at said second location to form a further focused second beam having a further focused second spot size that is smaller than the focused second spot size, wherein the first and third optical elements are at different spacial locations;

detecting at least a portion of the data in the further focused second beam.

24. A method, as claimed in claim 23, wherein the first optical element is a holographic unit.

25. A method, as claimed in claim 23, wherein the second optical element is a focusing element having a refractive index greater than 2.

26. A method, as claimed in claim 23, wherein:

said second focusing element reduces said focal spot size from a focal spot size diameter of greater than 100 microns to a focal spot size diameter of less than 50 microns.

27. A method, as claimed in claim 24, wherein:

said holographic unit includes at least one of the following;

a volume hologram and a holographic mirror.