Infrared Spatial Modulator for Non-Uniformity Correction

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Solution Overview

Problem

Heat-seeker missiles with IR thermal array sensors face non-uniformity issues due to varying responsitivity among pixels, leading to interference in guidance systems and the need for real-time correction to ensure accurate targeting.

Innovation Solution

A non-mechanical, scene-based non-uniformity correction system using an IR spatial modulator, such as smart glass, in the optical path of the IR sensor, which rapidly adjusts to provide uniform illumination and corrects for intensity variations by activating and deactivating to achieve real-time scene-based correction.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If traditional mechanical NUC methods are used, then non-uniformity correction can be achieved, but the correction process is slow and requires mechanical movement of components

Engineering Contradiction:
Improvecorrection speedVSAvoidmechanical component complexity
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

The patent replaces mechanical NUC methods with an optical-based solution using an IR spatial modulator that can rapidly change transmission properties without mechanical movement. The modulator uses electro-optic or liquid crystal effects to switch between transparent and scattering states, eliminating the need for mechanical shutters or moving parts while achieving faster correction speeds.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The IR spatial modulator provides dynamic control over the optical path by rapidly switching between transparent and scattering states. This dynamic capability allows the system to adapt to changing scene conditions in real-time, enabling correction speeds faster than mechanical systems can physically move components.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If pre-flight calibration is used, then non-uniformity correction can be performed, but it cannot adapt to in-flight conditions and requires separate calibration procedures

Engineering Contradiction:
Improvein-situ adaptation capabilityVSAvoidcalibration time
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The system performs self-calibration by using the scene itself as the calibration target. The IR spatial modulator scatters light from the actual scene to create a uniform reference pattern, allowing the system to automatically calculate and apply correction terms without external calibration equipment or pre-flight procedures. This eliminates calibration time loss during flight operations.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system prepares correction data by analyzing scattered scene light before final image capture. By pre-processing the scattered light patterns and calculating correction terms in advance, the system can rapidly apply corrections to the actual target image without delaying the overall operation.

Inventive Principle:
Principle #10Preliminary action

3Measurement precision

If the IR modulator is activated to scatter light for correction, then non-uniformity can be corrected, but the target image cannot be simultaneously captured

Engineering Contradiction:
Improveimage uniformityVSAvoidcorrection cycle time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The system uses rapid periodic switching of the IR spatial modulator between transparent and scattering states. This periodic action allows the system to quickly alternate between capturing scattered light for correction and capturing the actual target image, minimizing the time penalty of performing both functions.

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The scattered light pattern is captured and correction terms are calculated in advance before the final target image is captured. This preliminary processing of correction data allows the actual target imaging to proceed without delay, as the correction algorithms can be applied post-capture or during image processing.

Inventive Principle:
Principle #10Preliminary action

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables rapid, in situ non-uniformity correction in less than one second, improving the accuracy and sensitivity of the IR imaging system by providing a spatially corrected uniform image, enhancing the missile's ability to target effectively while reducing Fixed Pattern Noise.

Implementation Method 1

The IR modulator is capable of clearly transmitting and scattering variable intensities of IR radiation from a target imaged to the focal plane array (FPA) of a thermal IR sensor

Methodology Applied
Scientific EffectLight scattering: Scattering

Implementation Method 2

the IR modulator is made from a smart glass, such as a liquid crystal or suspended particle device, such as an electrochromic device

Methodology Applied
Scientific EffectElectro-optic effect: Electro-Optic Effects

Data Source

PatentUS8872111B2Infrared spatial modulator for scene-based non-uniformity image correction and systems and methods related thereto
Publication Date: 2014.10.28 RAYTHEON CO
  • US8872111B2 patent drawing
  • US8872111B2 patent drawing
  • US8872111B2 patent drawing

AI summary

Embodiments of an infrared spectral modulator for scene-based non-uniformity image correction are generally disclosed herein. The spectral modulator may be suitable for use in a system for navigating an object having a flight path comprising an infrared sensor having an optical path; an infrared modulator in the optical path of the infrared sensor, wherein the infrared modulator is configured to allow the infrared sensor to perform in situ, real-time, scene-based non-uniformity correction; and a guidance system within the object, wherein the guidance system can adjust the flight path of the object based on the non-uniformity correction.