Calibration system and method for lidar systems

• US 5,825,464 A
• Filed: 01/03/1997
• Issued: 10/20/1998
• Est. Priority Date: 01/03/1997
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Feichtner, John D.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US08/778,899
• Time in Patent Office: 655 Days
• Field of Search: 356/4.02, 356/6
• US Class Current: 356/4.02
• CPC Class Codes: G01S 7/4813 Housing arrangements
• CPC Class Codes: G01S 7/4818 using optical fibres
• CPC Class Codes: G01S 7/497 Means for monitoring or calibrating

Abstract

A calibration system and method include isotropically diffusing high-intensity light emitted from a detection apparatus, with the diffused light being coupled to at least one optical line, typically an optical fiber. In the preferred embodiment, the apparatus to be calibrated is a light detection and ranging (LIDAR) apparatus and the isotropic diffusion is achieved by means of an integrating sphere. For calibrating distance calculations, the optical fiber includes a reflecting mechanism, such as Bragg gratings, at a fixed and known distance from the input end of the optical fiber. The reflecting mechanisms simulates the presence of a remote object at the known distance. For a velocity calculation, a frequency offset may be introduced to the light propagating through the optical fiber, thereby simulating a Doppler shift induced by a moving object. The simulations of the presence and movement of remote objects are used to calibrate the apparatus.

Claims

1. A calibration system for a light-emitting apparatus which bases determinations relating to remote objects upon received backscattered light comprising:

an optical line having a first end;

reflective means connected to said line for inducing light reflection at a fixed distance from said first end of said optical line; and

distributing means for diffusing light emitted from said light-emitting apparatus substantially isotropically within a reflective cavity defined by said distributing means, said first end of said optical line being disposed relative to said reflective cavity to receive diffused light and to direct light reflected by said reflective means toward said distributing means for return to said light-emitting apparatus.

2. The calibration system of claim 1 wherein said distributing means is an integrating sphere and said optical line is a first optical fiber having said first end at a spherical wall of said integrating sphere, said reflective cavity being a substantially spherical interior of said integrating sphere.

3. The calibration system of claim 2 wherein said first optical fiber has a second end at said spherical wall such that said first optical fiber forms an optical loop.

4. The calibration system of claim 2 further comprising at least one second optical fiber having an end at said spherical wall, each second optical fiber having an associated reflective means for inducing light reflection at a second distance different than said fixed distance defined by said reflective means of said first optical fiber, said first and second optical fibers thereby simulating objects at different distances from said light-emitting apparatus.

5. The calibration system of claim 1 wherein said reflective means includes a first Bragg grating at said fixed distance from said first end of said optical line to simulate an object of interest in response to reflection of light by said first Bragg grating.

6. The calibration system of claim 5 further comprising a second Bragg grating along said optical line in spaced relation to said first Bragg grating to simulate a second object of interest in response to reflection of light by said second Bragg grating.

7. The calibration system of claim 1 further comprising a means along said optical line for shifting the frequency of said reflected light to simulate Doppler shifts initiated by moving objects.

8. The calibration system of claim 7 wherein said means for shifting the frequency is one of an acousto-optic modulator and an electro-optic modulator coupled to said optical line between said first end and said reflective means.

9. The calibration system of claim 1 wherein said optical line is a multimode optical fiber and said reflective means includes at least one Bragg grating along said multimode optical fiber.

10. A calibration system for a light detection and ranging (LIDAR) apparatus comprising:

an integrating sphere having an aperture aligned with said LIDAR apparatus to receive an incoming beam into a substantially spherical interior and to direct a return light signal to said LIDAR apparatus;

a plurality of optical fibers having first ends located at said integrating sphere such that each optical fiber is in optical communication with said substantially spherical interior; and

reflectors positioned along said optical fibers to reflect light propagating from said first ends for return to said substantially spherical interior, said reflected light forming said return light signal to said LIDAR apparatus.

11. The calibration system of claim 10 further comprising means along at least one of said optical fibers for modulating the frequency of light propagating through said at least one optical fiber, thereby simulating a Doppler shift.

12. The calibration system of claim 11 wherein said means for modulating includes an electrical signal generator connected to drive one of an acoustic-optic modulator and an electro-optic modulator coupled to said at least one optical fiber.

13. The calibration system of claim 10 wherein said substantially spherical interior of said integrating sphere has a diameter which is at least five times as great as a diameter of said aperture aligned with said LIDAR apparatus.

14. The calibration system of claim 10 wherein said reflectors are Bragg gratings.

15. A method of calibrating a light-emitting apparatus which bases determinations of ranges of remote objects upon received backscattered light comprising steps of:

positioning an output beam of said apparatus relative to an aperture of an integrating sphere such that said output beam impinges a substantially spherical interior surface of said integrating sphere, which substantially isotropically diffuses said output beam, thereby significantly attenuating light intensity;

simulating presence of a remote object at a known distance from said apparatus, including positioning a first end of an optical fiber relative to said surface to receive light from said surface and including reflecting said received light propagating through said optical fiber at a known position relative to said first end;

directing a return light signal from said surface to said apparatus such that said return light signal is representative of said light reflected at said known position of said optical fiber; and

adjusting a calculation of the distance of said simulated remote object from said apparatus to coincide with said known distance.

16. The method of claim 15 further comprising a step of simulating movement of said simulated remote object at a known velocity, including modulating the frequency of said light propagating through said optical fiber to simulate Doppler shifts.

17. The method of claim 16 further comprising a step of calibrating calculations of velocity of said simulated movements to coincide with said known velocity.

18. The method of claim 15 further comprising a step of simulating presence of at least one second remote object at a second known distance from said apparatus, including utilizing a corresponding number of second optical fibers.

19. The method of claim 15 wherein said step of simulating said presence of said remote object includes forming a Bragg grating along said optical fiber.