Offset aperture dual-gimbaled optical system

Patent metadata

Field	Value
Publication number	US-9347743-B2
Application number	US-201313944378-A
Country	US
Kind code	B2
Filing date	Jul 17, 2013
Priority date	Jul 17, 2013
Publication date	May 24, 2016
Grant date	May 24, 2016

Abstract

An offset aperture two-axis gimbaled optical system comprises a two-axis gimbal and an optics assembly that is mounted on the inner gimbal and offset radially from the rotation axis of the outer gimbal. The optics assembly is suitably offset so that its optical aperture does not overlap the rotation axis of the outer gimbal and its optical aperture is symmetric about the rotation axis of the inner gimbal. In different applications, the offset aperture provides for reduced optical aberrations and improved utilization of the available packaging volume to accommodate multiple offset aperture optics assemblies.

First claim

We claim:

1. A two-axis gimbaled optical system, comprising:
a dome that is symmetric about a first rotation axis;
an outer gimbal positioned behind the dome, said outer gimbal configured to rotate around the first rotation axis;
an inner gimbal mounted on the outer gimbal, said inner gimbal configured to rotate around a second rotation axis that is either perpendicular or skew to the first rotation axis; and
a first optics assembly mounted on the inner gimbal, said first optics assembly configured with an optical aperture offset radially from the first rotation axis and symmetric about the second rotation axis to receive optical radiation in a field-of-view (FOV) along a first optical axis, wherein rotation of said inner and outer gimbals about said second and first rotation axes traces the FOV over a field-of-regard (FOR) such that the FOV does not cross the central axis within the dome for any allowed rotation of the outer or inner gimbals,
wherein no optics assembly is mounted on the inner gimbal having a FOV that crosses the first rotation axis within the dome for any allowed rotation of the outer or inner gimbals.

2. The two-axis gimbaled optical system of claim 1 , wherein the conformal dome has a tip or extruded forebody that extends forward from the dome along the first rotation axis, wherein the FOV does not cross the tip or extruded forebody for any allowed rotation of the outer and inner gimbals.

3. The two-axis gimbaled optical system of claim 1 , further comprising:
a second optics assembly mounted on the inner gimbal to rotate about the second rotation axis, said second optics assembly configured with an optical aperture offset radially from the first rotation axis and symmetric about the second rotation axis to transmit or receive optical radiation in a FOV along a second optical axis, wherein rotation of the inner and outer gimbals traces the second optics assembly's FOV over a FOR such that the FOV does not cross the first rotation axis within the dome for any allowed rotation of the outer and inner gimbals.

4. The two-axis gimbaled optical system of claim 3 , wherein said first and said second axes lie in the same plane and are perpendicular to each other, wherein said first and second optics assemblies are offset radially along the second rotation axis on opposite sides of the first rotation axis.

5. The two-axis gimbaled optical system of claim 4 , further comprising:
a fixed optic assembly mounted off of the inner gimbal between said first and second optics assemblies, said fixed optic having a FOV that overlaps the central axis within the dome.

6. The two-axis gimbaled optical system of claim 1 , wherein said first and said second rotation axes lie in the same plane and are perpendicular to each other, wherein said first rotation axis is a roll axis and said rotation axis is a nod axis.

7. The two-axis gimbaled optical system of claim 6 , further comprising:
an off-gimbal optical component; and
a coudé path that optically couples the optics assembly on the inner gimbal to the off-gimbal optical component, said coudé path comprising a first fold mirror on the optics assembly to direct light along the second rotation axis and a second fold mirror at the intersection of the first and second rotation axes to direct light along the first rotation axis.

8. The two-axis gimbaled optical system of claim 1 , wherein said inner gimbal is offset radially on the outer gimbal.

9. The two-axis gimbaled optical system of claim 1 , wherein the dome comprises a conformal dome having curved inner and outer surfaces that are symmetric about the first rotation axis, further comprising:
an optical corrector mounted on said outer gimbal, said optical corrector adjacent the curved inner surface of the conformal dome in an optical path between the dome and the offset position of the first optics assembly's optical aperture that encompasses the FOV as the inner gimbal rotates about the second rotation axis, the optical corrector comprising an aspheric transparent arch having an optical corrector shape and position responsive to a shape of the dome at the offset position of the first optics assembly.

10. The two-axis gimbaled optical system of claim 9 , wherein said first and said second rotation axes lie in a plane and perpendicular to each other, wherein said optical corrector shape is a full-arch that is only symmetric about the plane.

11. The two-axis gimbaled optical system of claim 9 , wherein said first and second rotation axes are skew, wherein said optical corrector shape is approximately a half-arch that is only symmetric about a plane in which said first rotation axis lies and that is orthogonal to said second rotation axis.

12. The two-axis gimbaled optical system of claim 9 , wherein said first and second rotation axes are skew, wherein said optical corrector shape is a full arch that is asymmetric about all planes.

13. A two-axis gimbaled optical system, comprising:
a dome that is symmetric about a first rotation axis;
an outer gimbal positioned behind the dome, said outer gimbal configured to rotate around the first rotation axis;
one or more inner gimbals on the outer gimbal, said one or more inner gimbals configured to rotate around one or more inner rotation axes that are either perpendicular or skew to the first rotation axis;
a first optics assembly mounted on one of the inner gimbals, said first optics assembly configured with a first optical aperture offset radially from the first rotation axis and symmetric about its inner rotation axes to or receive optical radiation in a first field-of-view (FOV) along a first optical axis; and
a second optics assembly mounted on one of the inner gimbals, said second optics assembly configured with a second optical aperture offset radially from the first rotation axis and symmetric about its inner rotation axes to transmit or receive optical radiation in a second FOV along a second optical axis;
wherein rotation of the outer gimbal and the one or more inner gimbals traces the first and second FOV such that neither the first or second FOV cross the first rotation axis within the dome for any allowed rotation of the outer or one or more inner gimbals;
wherein no optics assembly is mounted on the inner gimbal having a FOV that crosses the first rotation axis within the dome for any allowable rotation of the outer or one or more inner gimbals.

14. The two-axis gimbaled optical system of claim 13 , wherein said first and second optics assemblies are mounted on ene the same inner gimbal.

15. The two-axis gimbaled optical system of claim 13 , wherein said first and second optics assemblies are mounted on different inner gimbals.

16. The two-axis gimbaled optical system of claim 13 , wherein said dome comprises a conformal dome having curved inner and outer surfaces that are symmetric about the first rotation axis, said inner and outer gimbals positioned behind the conformal dome, said optical system further comprising:
a first optical corrector mounted on said outer gimbal, said first optical corrector adjacent the curved inner surface of the conformal dome in an optical path between the dome and the offset position of first optics assembly's first optical aperture that encompasses the FOV as its inner gimbal rotates about its inner rotation axis, the first optical corrector comprising an aspheric transparent arch having an optical corrector shape and position responsive to a shape of the dome at the offset position of the first optics assembly; and
a second optical corrector mounted on said outer gimbal, said second optical corrector a

Assignees

• Raytheon Co

Inventors

• Martin Chadwick B
• Knapp David J
• Hanauska Gregory P

Classifications

• G02B27/0025

  for optical correction, e.g. distorsion, aberration · CPC title

• G02B26/101

  with both horizontal and vertical deflecting means, e.g. raster or XY scanners (colour television using laser beams scanning a display screen H04N9/3129) · CPC title

• F41G7/2293

  using electromagnetic waves other than radio waves · CPC title

• F41G7/22

  Homing guidance systems · CPC title

• F41G7/26

  Optical guidance systems · CPC title