Offset aperture gimbaled optical system with optically corrected conformal dome

Patent metadata

Field	Value
Publication number	US-9335126-B2
Application number	US-201313944267-A
Country	US
Kind code	B2
Filing date	Jul 17, 2013
Priority date	Jul 17, 2013
Publication date	May 10, 2016
Grant date	May 10, 2016

Abstract

An offset aperture gimbaled optical system comprises a gimbal and an optics assembly that is mounted on an inner gimbal and offset radially from an axis of symmetry (and rotation axis) of a conformal dome. An optical corrector adjacent the inner surface of the conformal dome encompasses the field-of-view of the optics assembly as the inner gimbal rotates about its rotation axis. The corrector is fixed with respect to the inner gimbal's rotation axis while it rotates about the axis of symmetry. The optical corrector comprises an aspheric transparent arch having an optical corrector shape and position responsive to a shape of the conformal dome at the offset position of the optics assembly. 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 gimbaled optical system comprising:
a conformal dome having curved inner and outer surfaces that are symmetrical about a first rotation axis;
an inner gimbal, said inner gimbal configured to rotate around a second rotation axis that is either perpendicular or skew to the first rotation axis;
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 to receive optical radiation in a first field-of-view (FOV) along a first optical axis, wherein rotation about said second and first rotation axes traces the first FOV over a field-of-regard (FOR) such that the FOV does not cross the first rotation axis within the dome for any allowed rotation;
a sensor optically coupled to the first optics assembly; and
a first 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 first FOV as the inner gimbal rotates about the second rotation axis, said first optical corrector configured to rotate about said first rotation axis with said first optics assembly and remain fixed with respect to said second 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;
wherein no optics assembly is mounted on the inner gimbal with an optical aperture to transmit or receive optical radiation in a FOV that crosses the first rotation axis within the dome for any allowed rotation.

2. A gimbaled optical system comprising:
a conformal dome having curved inner and outer surfaces that are symmetrical about a first rotation axis;
one or more inner gimbals, said one or more inner gimbals configured to rotate around one or more second rotation axes that are either perpendicular or skew to the first rotation axis;
a first optics assembly mounted on one of the one or more the inner gimbals, said first optics assembly configured with an optical aperture offset radially from the first rotation axis to transmit or receive optical radiation in a first field-of-view (FOV) along a first optical axis, wherein rotation about said second and first rotation axes traces the first FOV over a first field-of-regard (FOR) such that the first FOV does not cross the first rotation axis within the dome for any allowed rotation;
a second optics assembly mounted on one of the one or more the inner gimbals, said second optics assembly configured with an optical aperture offset radially from the first rotation axis to transmit or receive optical radiation in a second FOV along a second optical axis, wherein rotation about said second and first axes traces the second FOV over a second FOR such that the second FOV does not cross the first rotation axis within the dome for any allowed rotation;
a transmitter or sensor optically coupled to each said optics assembly; and
a first 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 first FOV as the inner gimbal rotates about the second rotation axis, said first optical corrector configured to rotate about said first rotation axis with said first optics assembly and remain fixed with respect to said second 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 adjacent the curved inner surface of the conformal dome in an optical path between the dome and the offset position of the second optics assembly's optical aperture that encompasses the second FOV as the inner gimbal rotates about the second rotation axis, said second optical corrector configured to rotate about said first rotation axis with said second optics assembly and remain fixed with respect to said second rotation axis, the second 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 second optics assembly;
wherein no optics assembly is mounted on the inner gimbal with an optical aperture to transmit or receive optical radiation in a FOV that crosses the first rotation axis within the dome for any allowed rotation.

3. A gimbaled optical system comprising:
a missile having a roll axis;
a conformal dome having curved inner and outer surfaces that are symmetrical about the roll axis;
an inner gimbal, said inner gimbal configured to rotate around a nod axis that is either perpendicular or skew to the roll axis;
a first optics assembly mounted on the inner gimbal, said first optics assembly configured with an optical aperture offset radially from the roll axis to receive optical radiation in a first field-of-view (FOV) along a first optical axis, wherein rotation about said roll and nod axes traces the first FOV over a field-of-regard (FOR) such that the FOV does not cross the roll axis within the dome for any allowed rotation;
a sensor optically coupled to the first optics assembly; and
a first 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 first FOV as the inner gimbal rotates about the first rotation axis, said first optical corrector configured to rotate about said roll axis with said first optics assembly and remain fixed with respect to said first 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;
wherein no optics assembly is mounted on the inner gimbal with an optical aperture to transmit or receive optical radiation in a FOV that crosses the roll axis within the dome for any allowed rotation.

4. The gimbaled optical system of claim 1 , wherein the inner gimbal, first optics assembly and first optical corrector are configured to rotate about said first rotation axis.

5. The gimbaled optical system of claim 1 , further comprising:
an outer gimbal configured to rotate about said first rotation axis, said inner gimbal mounted on the outer gimbal, said first optical corrector mounted on the outer gimbal to rotate about the first rotation axis.

6. The gimbaled optical system of claim 1 , wherein said optical aperture is symmetric about the second rotation axis.

7. The gimbaled optical system of claim 1 , further comprising:
a second optics assembly mounted on the inner gimbal, said second optics assembly configured with an optical aperture offset radially from the first rotation axis to transmit or receive optical radiation in a second FOV along a second optical axis, wherein rotation about said second and first rotation axes traces the second FOV over a second FOR such that the second FOV does not cross the first rotation axis within the dome for any allowed rotation; and
a second optical corrector adjacent the curved inner surface of the conformal dome in an optical path between the dome and the offset position of the second optics assembly's optical aperture that encompasses the second FOV as the inner gimbal rotates about the second rotation axis, said second optical corrector configured to rotate about said first rotation axis with said second optics assembly and remain fixed with respect to said second rotation axis, the secon

Assignees

• Raytheon Co

Inventors

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

Classifications

• 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

• F41G7/2213 Primary

  maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro · CPC title

• G02B27/0037

  with diffracting elements (G02B27/0056 takes precedence; holographic optical elements G02B5/32; zone systems G02B5/1876) · CPC title

• F41G7/26

  Optical guidance systems · CPC title