Fiber optic guidance system for laser guided missiles

• US 5,784,156 A
• Filed: 11/19/1996
• Issued: 07/21/1998
• Est. Priority Date: 11/19/1996
• Status: Expired due to Term

• Current Assignee: BAE Systems Information and Electronic Systems Integration Incorporated (BAE Systems Plc)
• Original Assignee: Tracor Aerospace, Inc. (BAE Systems Plc)
• Inventors: Nicholson, James E.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US08/752,326
• Time in Patent Office: 609 Days
• Field of Search: 356/141.5, 385/116, 244/3.16
• US Class Current: 356/141.5
• CPC Class Codes: F41G 7/226 Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
• CPC Class Codes: F41G 7/2293 using electromagnetic waves other than radio waves
• CPC Class Codes: G01S 3/783 using amplitude comparison of signals derived from static detectors or detector systems

Abstract

The invention provides a system and a method for determining the direction to a radiating source, for use by a vehicle guidance system, in which optical fibers are used to both collect and transmit optical signals in which the vehicle is preferably intended to home in on its target. The optical fibers disclosed herein require no separate collection optics, but instead directly collect incident radiation arriving at one end of the optical fiber for transmission to a photodiode detector coupled to the distal end. Preferably the radiation is laser radiation radiating from a target in relation to which the vehicle is guided, and preferably the vehicle is a guided missile. Elimination of collection optics reduces the complexity and cost of the apparatus and provides an unexpected increase in and selectability of the accuracy of directional determination by the system. The system includes an array of apertures disposed in selected, non-uniform locations on the vehicle. Each aperture contains a set of fibers, including start and stop fibers. The fibers receive incoming radiation, transmit the radiation as optical signals to start and stop detectors. The detectors measure a signal strength and a property related to the length of the start and stop fibers through which the optical signals have been transmitted, and provide output indicative of the signal strength and the property to a microprocessor. The microprocessor is programmed to calculate the direction to the radiation source relative to the vehicle, and to provide this information to a vehicle guidance and control system.

Claims

1. A system for determining the direction to a radiating source relative to a moving vehicle deploying the system and for providing information to a guidance system for the vehicle, by reference to an optical source signal received from the radiating source at a subarray of apertures, the system comprising:

an array of apertures arrayed at selected positions on the vehicle;

a plurality of start optical fibers, each start optical fiber having substantially the same length, each start fiber having a first, radiation receiving end and a second end coupled to a start detector;

a plurality of stop optical fibers, each stop fiber having a selected length equal to or greater than the length of the start fibers, each stop fiber having a first, radiation receiving end and a second end coupled to a stop detector,

one start fiber and at least one stop fiber being coupled together to form a set of fibers, one set of fibers being disposed at each aperture, all the fibers in each set of fibers having the same selected numerical aperture and being directed in the same selected direction relative to the vehicle, and the apertures having a selected degree of overlap with adjacent apertures;

the first radiation receiving end of each set of fibers adapted to receive the optical source signal for transmission as an optical signal to the detector coupled thereto;

each detector being adapted to detect and measure the optical signal strength of the optical signal arriving on the fibers coupled thereto, adapted to produce a strength output signal related to the optical signal strength of each optical signal, and adapted to provide the strength output signal to a microprocessor;

the start detector being adapted to measure a property and produce a start output signal related to the length of the start fiber through which the optical signal has been transmitted;

the stop detector being adapted to measure the property and produce a stop output signal related to the length of the stop fiber through which the optical signal has been transmitted;

wherein the start output signal and the stop output signal provide input to a device which measures a difference in the apparent phase between the start output signal and the stop output signal, and provides information on this difference to the microprocessor, the microprocessor being programmed to calculate the direction to the radiating source from the strength output signal and the difference in the apparent phase of the start and stop signals.

2. A system as claimed in claim 1, wherein the first light receiving end of each optical fiber includes no separate light gathering apparatus.

3. A system as claimed in claim 1, wherein the vehicle is a guided missile and the source signal is laser light reflected from a target toward which the missile is directed.

4. A system as claimed in claim 3, wherein the laser light is in a spectral range from ultraviolet to far infrared light.

5. A system as claimed in claim 1, wherein the at least one stop fiber in the set of fibers includes an azimuth stop fiber and an elevation stop fiber, the azimuth stop fiber being coupled to an azimuth stop detector, and the elevation stop fiber being coupled to an elevation stop detector.

6. A system as claimed in claim 5, wherein the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

7. A system as claimed in claim 1, wherein each stop fiber in the set of fibers includes a splitter for splitting the optical signal into at least two portions, in which one portion is an azimuth stop signal carried to an azimuth stop detector and one portion is an elevation stop signal carried to an elevation stop detector.

8. A system as claimed in claim 7, wherein the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

9. A system as claimed in claim 1, wherein each fiber includes a splitter for splitting the optical signal into three portions, in which one portion is a start signal carried to the start detector, one portion is an azimuth stop signal carried to an azimuth stop detector, and one portion is an elevation stop signal carried to an elevation stop detector, the three portions comprising a set of fibers.

10. A system as claimed in claim 9, wherein the start detector measures the property and produces a start output signal related to the length of the start fiber through which the optical signal has been transmitted, the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

11. A system as claimed in claim 1, wherein the set of fibers comprises an integral multiple of start fibers, an equivalent number of azimuth stop fibers, and an equivalent number of elevation stop fibers.

12. A system as claimed in claim 11, wherein the range of integral multiples is from 2 to 100 fibers.

13. A system as claimed in claim 12, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of azimuth stop fibers, and a number of elevation stop fibers equivalent to the number of azimuth stop fibers.

14. A system as claimed in claim 12, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of azimuth stop fibers, and a number of elevation stop fibers greater than the number of start fibers but less than the number of azimuth stop fibers.

15. A system as claimed in claim 12, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of elevation stop fibers, and a number of azimuth stop fibers greater than the number of start fibers but less than the number of elevation stop fibers.

16. A method for determining the direction to a radiating source relative to a moving vehicle deploying the system and for providing directional information to a guidance system for the vehicle, by reference to an optical source signal received from the radiating source at a subarray of apertures, the method comprising the steps of:

arraying a plurality of apertures at selected positions on the vehicle,

providing a plurality of start optical fibers, each start optical fiber having substantially the same length, each start fiber having a first, radiation receiving end and a second end coupled to a start detector;

providing a plurality of stop optical fibers, each stop fiber having a selected length equal to or greater than the length of the start fibers, each stop fiber having a first, radiation receiving end and a second end coupled to a stop detector,

one start fiber and at least one stop fiber being coupled together to form a set of fibers, one set of fibers being disposed at each aperture, all the fibers in each set of fibers having the same numerical aperture and being directed in the same direction relative to the vehicle, and the first radiation receiving end of each set of fibers receiving the optical source signal for transmission as an optical signal to the detector coupled thereto;

each detector detecting and measuring the optical signal strength of the optical signal arriving on the fibers coupled thereto, producing a strength output signal related to the optical signal strength of each optical signal, and providing the strength output signal to a microprocessor programmed to calculate the direction to the radiating source;

the start detector producing a start output signal related to the length of the start fiber through which the optical signal was transmitted;

the stop detector producing a stop output signal related to the length of the stop fiber through which the optical signal was transmitted;

providing input to a device measuring an apparent phase difference between the start output signal and the stop output signal, and providing information on the difference to the microprocessor,

calculating with the microprocessor the direction to the radiating source from the strength output signal and the apparent phase difference between the start output signal and the stop output signal.

17. A method as claimed in claim 16, wherein the first light receiving end of each optical fiber includes no separate light gathering apparatus.

18. A method as claimed in claim 16, wherein the vehicle is a guided missile and the source signal is laser light reflected from a target toward which the missile is directed.

19. A method as claimed in claim 18, wherein the laser light is in a spectral range from ultraviolet to far infrared light.

20. A method as claimed in claim 16, wherein the at least one stop fiber in the set of fibers includes an azimuth stop fiber and an elevation stop fiber, the azimuth stop fiber being coupled to an azimuth stop detector, and the elevation stop fiber being coupled to an elevation stop detector.

21. A method as claimed in claim 20, wherein the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

22. A method as claimed in claim 16, wherein each stop fiber in the set of fibers includes a splitter for splitting the optical signal into at least two portions, in which one portion is an azimuth stop signal carried to an azimuth stop detector and one portion is an elevation stop signal carried to an elevation stop detector.

23. A method as claimed in claim 22, wherein the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

24. A method as claimed in claim 16, wherein each fiber includes a splitter for splitting the optical signal into three portions, in which one portion is a start signal carried to the start detector, one portion is an azimuth stop signal carried to an azimuth stop detector, and one portion is an elevation stop signal carried to an elevation stop detector, the three portions comprising a set of fibers.

25. A method as claimed in claim 24, wherein the start detector measures the property and produces a start output signal related to the length of the start fiber through which the optical signal has been transmitted, the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

26. A method as claimed in claim 16, wherein the set of fibers comprises an integral multiple of start fibers, an equivalent number of azimuth stop fibers, and an equivalent number of elevation stop fibers.

27. A method as claimed in claim 26, wherein the range of integral multiples is from 2 to 100 fibers.

28. A method as claimed in claim 27, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of azimuth stop fibers, and a number of elevation stop fibers equivalent to the number of azimuth stop fibers.

29. A method as claimed in claim 27, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of azimuth stop fibers, and a number of elevation stop fibers greater than the number of start fibers but less than the number of azimuth stop fibers.

30. A method as claimed in claim 27, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of elevation stop fibers, and a number of azimuth stop fibers greater than the number of start fibers but less than the number of elevation stop fibers.

31. A method as claimed in claim 16, wherein the steps of providing a plurality of start and stop optical fibers includes selecting the numerical aperture for the set of fibers.

32. A method as claimed in claim 16, wherein the steps of providing a plurality of start and stop optical fibers includes selecting the degree of overlap between fibers in adjacent apertures.

33. A method as claimed in claim 16, wherein the steps of providing a plurality of start and stop optical fibers includes selecting the number of apertures arrayed in each selected direction.

34. A system for determining the direction to a radiating source relative to a moving vehicle deploying the system and for providing information to a guidance system for the vehicle, by reference to an optical source signal received from the radiating source at a subarray of apertures, the system comprising:

an array of apertures, arrayed at selected locations on the vehicle;

a plurality of first and second optical fibers, each optical fiber being provided with no separate light gathering device, each optical fiber being capable of detecting laser radiation over a certain field of view, the field of view of each optical fiber overlapping the field of view of its neighbors, with all first optical fibers being of substantially the same length and the lengths of the second optical fibers being of equal or greater length in order to form different transit times, and at least one first optical fiber and at least one second optical fiber forming a set of fibers at each aperture, each set of fibers having substantially the same field of view and being directed in the same direction;

first and second detectors having opto-electrical transducers and coupled respectively to the first and second wave guides;

each detector being adapted to detect and measure the optical signal strength of the optical signal arriving on the fibers coupled thereto, adapted to produce a strength output signal related to the optical signal strength of each optical signal, and adapted to provide the strength output signal to a microprocessor;

the first detector being adapted to produce a first output signal related to the length of the first optical fiber through which the optical signal has been transmitted;

the second detector being adapted to produce a second output signal related to the length of the second fiber through which the optical signal has been transmitted;

wherein the first output signal and the second output signal provide input to a device which measures an apparent phase difference between the first output signal and the second output signal, and provides information on this difference to the microprocessor, the microprocessor being programmed to calculate the direction to the radiating source from the strength output signal and the apparent phase difference between the start and stop signals.

35. A system as claimed in claim 34, wherein the vehicle is a guided missile and the source signal is laser light reflected from a target toward which the missile is directed.

36. A system as claimed in claim 35, wherein the laser light is in a spectral range from ultraviolet to far infrared light.

37. A system as claimed in claim 34, wherein the at least one stop fiber in the set of fibers includes an azimuth stop fiber and an elevation stop fiber, the azimuth stop fiber being coupled to an azimuth stop detector, and the elevation stop fiber being coupled to an elevation stop detector.

38. A system as claimed in claim 37, wherein the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

39. A system as claimed in claim 34, wherein each stop fiber in the set of fibers includes a splitter for splitting the optical signal into at least two portions, in which one portion is an azimuth stop signal carried to an azimuth stop detector and one portion is an elevation stop signal carried to an elevation stop detector.

40. A system as claimed in claim 39, wherein the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

41. A system as claimed in claim 34, wherein each fiber includes a splitter for splitting the optical signal into three portions, in which one portion is a start signal carried to the start detector, one portion is an azimuth stop signal carried to an azimuth stop detector, and one portion is an elevation stop signal carried to an elevation stop detector, the three portions comprising a set of fibers.

42. A system as claimed in claim 41, wherein the start detector measures the property and produces a start output signal related to the length of the start fiber through which the optical signal has been transmitted, the azimuth stop detector measures the property and produces an azimuth stop output signal related to the length of the azimuth stop fiber through which the optical signal has been transmitted, and the elevation stop detector measures the property and produces an elevation stop output signal related to the length of the elevation stop fiber through which the optical signal has been transmitted.

43. A system as claimed in claim 34, wherein the set of fibers comprises an integral multiple of start fibers, an equivalent number of azimuth stop fibers, and an equivalent number of elevation stop fibers.

44. A system as claimed in claim 43, wherein the range of integral multiples is from 2 to 100 fibers each of start fibers, azimuth stop fibers, and elevation stop fibers.

45. A system as claimed in claim 34, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of azimuth stop fibers, and a number of elevation stop fibers equivalent to the number of azimuth stop fibers.

46. A system as claimed in claim 34, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of azimuth stop fibers, and a number of elevation stop fibers greater than the number of start fibers but less than the number of azimuth stop fibers.

47. A system as claimed in claim 34, wherein the set of fibers comprises an integral multiple of start fibers, a greater number of elevation stop fibers, and a number of azimuth stop fibers greater than the number of start fibers but less than the number of elevation stop fibers.