Light source characterization system
Various measurement systems and methods are disclosed to enable characterizing the optical characteristics of light beams emitted by a light detection and range finding (LIDAR) system or sensor and evaluating the range finding function of user selected lidar channels while the lidar operates under a real operational condition and is exposed to a range of user defined environmental conditions.
1 . A system, comprising:
a housing configured to house a light source within a cavity formed by the housing, wherein the housing comprises;
an internal surface of the cavity surrounding the light source, the internal surface configured to reflect light beams emitted by the light source,
a first aperture configured to enable a first at least one light beam to exit the cavity along a straight optical path from the light source passing through the first aperture, wherein the first at least one light beam is emitted by the light source during a first portion of a rotational period of the light source,
a second aperture configured to enable a second at least one light beam to exit the cavity, wherein the second at least one light beam is emitted by the light source during a second portion of the rotational period of the light source and reflected by the internal surface; and
at least one optical guard housed in the cavity and configured to interact with a third at least one light beam from the light source, wherein the third at least one light beam is emitted by the light source during the first portion of the rotational period of the light source.
2 . The system of claim 1 , wherein the second at least one light beam is reflected multiple times by the internal surface before exiting the cavity via the second aperture.
3 . The system of claim 1 , wherein the at least one optical guard comprises an optically reflective surface configured to reflect the third at least one light beam towards the first aperture.
4 . The system of claim 1 , wherein the at least one optical guard comprises an absorptive surface configured to absorb the third at least one light beam.
5 . The system of claim 1 , wherein the cavity is a spherical cavity.
6 . The system of claim 1 , wherein the second portion of the rotational period is longer than the first portion of the rotational period.
7 . The system of claim 1 , further comprising a temperature control system configured to control a temperature of an internal volume of the cavity, the temperature control system comprising:
a thermometer configured to measure the temperature of the internal volume of the cavity;
an air conditioner configured to change the temperature of the internal volume of the cavity; and
a controller configured to control the air conditioner based at least in part on the measured temperature of the internal volume of the cavity.
8 . The system of claim 7 , further comprising a humidity control system configured to control a humidity of the internal volume of the cavity, the humidity control system comprising:
a humidity measurement device configured to measure the humidity in the internal volume of the cavity;
a humidity control device configured to change the humidity in the internal volume of the cavity; and
a controller configured to control the humidity control device based at least in part on the measured humidity in the internal volume of the cavity.
9 . The system of claim 1 , wherein the first aperture extends in a longitudinal direction from a top edge to a bottom edge on the internal surface along a polar direction, and wherein the at least one optical guard is positioned proximate the top edge or the bottom edge.
10 . The system of claim 1 , further comprising a measurement device configured to receive the second at least one light beam through the second aperture.
11 . The system of claim 10 , wherein the measurement device comprises an optical spectrum analyzer configured to measure an optical spectrum of the second at least one light beam.
12 . The system of claim 10 , wherein the measurement device comprises an optical power meter configured to measure an average optical power of light emitted by the light source during the second portion of the rotational period.
13 . The system of claim 1 , wherein the light source, is configured to emit light at different rotational positions with respect to a rotational axis, and wherein at a particular rotational position the light source emits a plurality of light beams at different directions about an emission axis perpendicular to the rotational axis.
14 . The system of claim 13 , wherein the light source comprises a laser range finder, and the light source is further configured to receive reflected light beams associated with the plurality of light beams.
15 . The system of claim 14 , wherein the reflected light beams are received from an object exterior to the cavity, wherein the object is configured to reflect the first at least one light beam towards the first aperture.
16 . The system of claim 15 , wherein the light source is configured to receive reflection of the first at least one light beam from the object via a direct optical path passing through the first aperture, during the first portion of the rotational period.
17 . The system of claim 16 , wherein the light source does not receive light associated with the third at least one light beam.
18 . The system of claim 13 , wherein the plurality of light beams are emitted by a plurality of channels of the light source, and wherein the first at least one light beam is emitted by a selected channel of the plurality of channels.
19 . The system of claim 18 , wherein the system comprises a rotational stage positioned inside the cavity, wherein the light source is mounted on the rotational stage and the rotational stage is configured to rotate the light source around a channel selection axis perpendicular to the rotational axis.
20 . The system of claim 19 , wherein the rotational stage is further configured to align the first at least one light beam with the first aperture to allow the first at least one light beam to directly exit the cavity through the first aperture.
21 . The system of claim 19 , wherein the selected channel is selected using the rotational stage.
22 . The system of claim 1 , wherein the internal surface comprises a diffuse reflective surface.
23 . The system of claim 22 , wherein the second at least one light beam is diffusively reflected by the internal surface.