Liquid crystal waveguide steered active situational awareness sensor

Patent metadata

Field	Value
Publication number	US-9927515-B2
Application number	US-201514748928-A
Country	US
Kind code	B2
Filing date	Jun 24, 2015
Priority date	Jun 24, 2015
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

An active situational sensor achieves SWaP-C and SNR improvements by using a liquid crystal waveguide to steer a spot-beam onto a conical shape of a fixed mirror, which redirects the spot-beam to scan a FOV. The sensor may rapidly scan a 360° horizontal FOV with a specified vertical FOV or any portion thereof, jump discretely between multiple specific objects per frame, vary the dwell time on an object or compensate for other external factors to tailor the scan to a particular application or changing real-time conditions. The sensor can be used to provide object intensity or ranging in complex, dynamic systems such as aviation, air traffic control, ship navigation, unmanned ground vehicles, collision avoidance, object targeting etc.

First claim

We claim:

1. A situational awareness sensor, comprising:
a laser configured to generate a collimated spot-beam along an optical axis that is oriented in the Z direction;
a liquid crystal waveguide (LCWG) along the optical axis responsive to command signals to steer the spot-beam about the optical axis to a location Theta X and Theta Y from the optical axis where Theta X is the angle between the projection of the instantaneous location of the axis of spot-beam on the X-Z plane and the Z axis and Theta Y is the angle between the instantaneous location of the axis of the spot-beam on the Y-Z plane and the Z axis, Theta Z is the angle between the projection of the instantaneous location of the axis of the steered spot-beam and the Z axis;
a controller configured to issue command signals to the LCWG to steer the spot-beam to the desired Theta X and Theta Y;
a fixed mirror having a conical shape oriented along the optical axis that redirects the spot-beam to a location Phi and Theta Z′ where Phi is the angle between the projection of the instantaneous location of the axis of the redirected spot-beam on the X-Y plane and the X axis and Theta Z′ is the angle between the projection of the instantaneous location of the axis of redirected spot-beam on the Z axis and Theta Z′ is greater than Theta Z, wherein the redirected spot-beam scans a field-of-view (FOV) defined by the values of Phi and Theta Z′; and
a detector configured to sense a reflected component of the spot-beam.

2. The sensor of claim 1 , wherein an angle Theta F of the conical shape of the fixed mirror is configured to redirect the spot-beam perpendicular to the optical axis.

3. The sensor of claim 1 , wherein the conical shape of the fixed mirror is a normal cone in which the surface of the cone is rotationally symmetric about the optical axis.

4. The sensor of claim 1 , wherein the conical shape is a piecewise linear approximation of a cone in which the base of the cone is represented by a polygon.

5. The sensor of claim 1 , wherein the conical shape includes an aspheric curvature.

6. The sensor of claim 1 , wherein the conical shape includes an optic L 1 to focus the spot-beam on the conical shape.

7. The sensor of claim 1 , further comprising an optic L 1 between the LCWG and the fixed mirror to focus the collimated spot-beam onto the conical shape of the fixed mirror.

8. The sensor of claim 7 , further comprising
a structural member configured to provide support primarily in the direction parallel to the sensor axis, said structural support having N discrete apertures formed therein at 360/N degree intervals; and
N transport optic channels placed around the fixed mirror at 360/N degree intervals, each channel comprising an optic L 2 configured to collimate the redirected spot-beam and an optic L 3 configured to direct the collimated redirected spot-beam through the corresponding aperture.

9. The sensor of claim 1 , wherein the controller issues command signals to steer the spot-beam in a circle around the conical shape and to vary the radius of the circle to move back-and-forth on the conical shape along the optical axis to scan a 360 degree region in phi and a defined FOV in the X-Y plane.

10. The sensor of claim 9 , wherein an angle Theta F of the conical shape of the fixed mirror is configured to redirect the spot-beam perpendicular to the optical axis such that the spot-beam scans a 360 degree horizontal FOV and a defined vertical FOV.

11. The sensor of claim 1 , wherein the controller issues command signals to steer the spot-beam to discrete theta X and theta Y to cause the redirected spot-beam to jump between multiple discrete objects in the FOV.

12. The sensor of claim 11 , wherein the controller issues command signals to illuminate multiple discrete objects within a single frame time.

13. The sensor of claim 11 , wherein the controller issues command signals to vary the dwell times on different discrete objects.

14. The sensor of claim 1 , wherein the controller issues command signals in an acquisition mode to scan a defined FOV to acquire objects and then issues command signals to move the spot-beam discretely from one object to the next to track multiple objects per frame.

15. The sensor of claim 1 , wherein the controller issues command signals responsive to an external signal to remove the effects of the external signal to maintain the scan of the FOV or object.

16. A situational awareness sensor, comprising:
a laser configured to generate a collimated spot-beam along an optical axis that is oriented in the Z direction;
a liquid crystal waveguide (LCWG) along the optical axis responsive to command signals to steer the spot-beam about the optical axis to a location Theta X and Theta Y from the optical axis where Theta X is the angle between the projection of the instantaneous location of the axis of spot-beam on the X-Z plane and the Z axis and Theta Y is the angle between the instantaneous location of the axis of the spot-beam on the Y-Z plane and the Z axis, Theta Z is the angle between the projection of the instantaneous location of the axis of the steered spot-beam and the Z axis;
a controller configured to issue command signals to the LCWG to steer the spot-beam to the desired Theta X and Theta Y;
an optic L 1 that focuses the collimated spot-beam
a fixed mirror having a conical shape that is rotationally symmetric about the optical axis that redirects the focused spot-beam perpendicular to the optical axis to a location Phi and Theta Z′ where Phi is the angle between the projection of the instantaneous location of the axis of the redirected spot-beam on the X-Y plane and the X axis and Theta Z′ is the angle between the projection of the instantaneous location of the axis of redirected spot-beam on the Z axis and Theta Z′ is greater than Theta Z;
a structural member configured to provide support primarily in the direction parallel to the sensor axis, said structural member having N discrete apertures formed therein at 360/N degree intervals;
N transport optic channels placed around the fixed mirror at 360/N degree intervals, each channel comprising an optic L 2 configured to collimate the redirected spot-beam and an optic L 3 configured to direct the collimated redirected spot-beam through the corresponding aperture such that the redirected spot-beam scans a field-of-view (FOV) defined by the values of Phi and Theta Z′; and
a detector configured to sense a reflected component of the spot-beam.

17. A situational awareness sensor, comprising:
a laser configured to generate a collimated spot-beam along an optical axis;
a liquid crystal waveguide (LCWG) along the optical axis responsive to command signals to steer the spot-beam in two-dimensions about the optical axis;
a controller configured to issue command signals to the LCWG to steer the spot-beam;
a fixed mirror having a conical shape oriented along the optical axis that redirects the spot-beam to scan a two-dimensional field-of-view (FOV); and
a detector configured to sense a reflected component of the spot-beam.

18. The sensor of claim 17 , further comprising an optic L 1 between the LCWG and the fixed mirror to focus the collimated spot-beam onto the conical shape of the fixed mirror.

19. The sensor of claim 17 , further comprising
a structural member configured to provide support primarily in the direction parallel to the sensor axis, said structural member having N discrete apertures formed therein at 360/N degree intervals; and
N transport optic channels placed around the fixed mir

Assignees

• Raytheon Co

Inventors

• Keller Sean D
• Uyeno Gerald P

Classifications

• G01S7/4817 Primary

  relating to scanning · CPC title

• G01S17/42

  Simultaneous measurement of distance and other co-ordinates (indirect measurement G01S17/46) · CPC title

• G02F1/29

  for the control of the position or the direction of light beams, i.e. deflection · CPC title