Wing mounted seeker

Patent metadata

Field	Value
Publication number	US-11168959-B2
Application number	US-201916527112-A
Country	US
Kind code	B2
Filing date	Jul 31, 2019
Priority date	Jul 31, 2019
Publication date	Nov 9, 2021
Grant date	Nov 9, 2021

Abstract

An optical seeker assembly having an optical detector located within the wing or canards of a precision guided munition. The optical seeker provides on-wing processing that generates low bandwidth detection data that can be easily transferred to a primary CPU located within the main body or fuselage of the precision guided munition. The on-wing processing reduces or eliminates the need for optical fibers extending between an optical wedge and an optical detector to reduce the likelihood of optical fibers from impeding in the mechanical deployment of the wing and reduces losses. The reduction or elimination of optical fibers between the optical wedge and the optical detector further enables the optical detection assembly to have a higher pixel ratio or transmitting raw data between the wedge and the detector by sending sampled detection data across a low bandwidth link to a CPU in the main body.

First claim

The invention claimed is:

1. An optical seeker assembly for a precision guided munition, the optical seeker assembly comprising:
an optical waveguide configured to transmit an optical signal therethrough; and
an optical detector coupled to the optical waveguide to detect the optical signal transmitted through the optical waveguide,
wherein the optical waveguide and the optical detector move in unison being carried by a wing of the precision guided munition as the wing moves from a first position to a deployed second position.

2. The optical seeker assembly of claim 1 , further comprising:
a first end of the optical waveguide that is sized complementary to an aperture formed in a leading edge of the wing; and
a second end of the optical waveguide disposed forwardly from a trailing edge of the wing, wherein the optical detector is connected to the second end of the optical waveguide and the optical detector is positioned forwardly from the trailing edge within the wing.

3. The optical seeker assembly of claim 2 , further comprising:
a circuit card in electrical communication with the optical detector for processing a plurality of pulses detected by the optical detector, wherein the circuit card has a rear edge disposed forwardly from the trailing edge within the wing.

4. The optical seeker assembly of claim 3 , further comprising:
a low bandwidth link between the wing and a body of platform to which the wing is moveably connected; and
a pulse discriminator mounted within the wing electrically coupled to the circuit card for converting the pulses into low bandwidth signals for transmission along the low bandwidth link from the wing to a main processor within the body of the platform.

5. The optical seeker assembly of claim 1 , wherein the optical seeker assembly is free of any fiber optic cables that extend from the wing into a main body to which the wing is moveably connected.

6. The optical seeker assembly of claim 3 , further comprising a pulse discriminator, wherein the pulse discriminator is a field programmable gate array (FPGA) within the wing that down samples processed pulse data from the circuit card into the low bandwidth signal for transmission along the low bandwidth link in the form of a wire harness that does not inhibit the movement of the wing between the first and second positions.

7. The optical seeker assembly of claim 3 , wherein the circuit card comprises:
a transimpedance amplifier
a high pass filter electrically downstream from the transimpedance amplifier;
a variable gain amplifier electrically downstream from the high pass filter; and
an analog-to-digital converter electrically downstream from the variable gain amplifier.

8. The optical seeker assembly of claim 7 , further comprising:
a flexible circuit coupling an output of the optical detector to an input of the transimpedance amplifier, wherein the flexible circuit is disposed entirely within the wing.

9. The optical seeker assembly of claim 1 , further comprising:
a longitudinal axis of the optical waveguide; and
a circuit card mounted within the wing in electrical communication with the optical detector, wherein the circuit card has a first major surface that does not intersect the longitudinal axis of the optical waveguide within the wing.

10. The optical seeker assembly of claim 1 , further comprising:
a lens that focuses light in one dimension;
a narrow passband optical filter matching designator wavelength; and
an optical epoxy that mounts the optical detector directly to the optical waveguide.

11. The optical seeker assembly of claim 1 , further comprising:
a phase change material within a housing exterior to the optical waveguide adapted to ensure that the optical detector temperature is maintained within an operational range during a transitory event that affects thermal environment; and
a reflective coating on the optical waveguide.

Assignees

• Bae Sys Inf & Elect Sys Integ

Inventors

• Frey Jr Robert D
• Affleck Maxwell L
• Batchelder Jason H
• Cullen Joseph P
• Robichaud Matthew H

Classifications

• G01J1/0422

  using light concentrators, collectors or condensers · CPC title

• G01J1/0407

  Optical elements not provided otherwise, e.g. manifolds, windows, holograms, gratings · CPC title

• G01J1/0252

  Constructional arrangements for compensating for fluctuations caused by, e.g. temperature, or using cooling or temperature stabilization of parts of the device; Controlling the atmosphere inside a photometer; Purge systems, cleaning devices (protection against electromagnetic interferences G01J2001/0276) · CPC title

• G01J1/0219 Primary

  Electrical interface; User interface · CPC title

• G01J1/0214

  Constructional arrangements for removing stray light · CPC title