Sun-Tracking Mirror for Airborne Imaging Calibration

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Solution Overview

Problem

Existing location markers for satellite imaging systems are large and static, occupying significant land area and requiring satellite maneuvers for calibration, which limits their practicality and accuracy.

Innovation Solution

A compact, mobile location marker system using a mirror capable of tilting about orthogonal axes to track the sun and reflect its beam towards the satellite, allowing for precise calibration of spatial coordinates without the need for satellite adjustments, utilizing a camera to obtain transformation of mirror axes and determine a known earth reference location within aerial images.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If large static resolution targets are used as location markers, then the markers are visible to airborne cameras and enable accurate calibration, but the markers occupy large land area and require satellite maneuvers

Engineering Contradiction:
Improvecalibration accuracyVSAvoidland area occupied
Core Design Contradiction:
Measurement precisionVSArea of stationary object

Solution Approach 1:

The invention changes the fundamental parameter of the location marker from a large static target to a compact mobile mirror. The mirror's small size dramatically reduces land area occupation, while its mobility and sun-tracking capability maintain visibility to airborne cameras. The mirror reflects sunlight to create a visible reference point without requiring large physical dimensions.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The invention transitions from static location markers to a dynamic mobile mirror system. The mirror can move and reposition itself, eliminating the need for satellite maneuvers to achieve proper calibration geometry. The mirror's ability to track the sun and adjust its position provides dynamic adaptability while maintaining calibration accuracy.

Inventive Principle:
Principle #15Dynamics

2Measurement precision

If large static resolution targets are used as location markers, then the markers are visible to airborne cameras, but the satellite must undertake special maneuvers to track the markers

Engineering Contradiction:
Improvecalibration accuracyVSAvoidoperational complexity
Core Design Contradiction:
Measurement precisionVSEase of operation

Solution Approach 1:

The mobile mirror system dynamically adjusts its position and orientation to maintain visibility and proper calibration geometry with the airborne camera. The mirror tracks the sun and can reposition itself, eliminating the need for complex satellite maneuvers. This dynamic adaptability simplifies the operational process while maintaining calibration accuracy.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The mirror system serves itself by autonomously tracking the sun and adjusting its position to remain visible to the airborne camera. This self-service capability eliminates the need for complex coordinated maneuvers between the satellite and ground equipment, reducing operational complexity while maintaining calibration precision.

Inventive Principle:
Principle #25Self-service

3Area of stationary object

If compact location markers are used, then land area occupancy is reduced, but the markers may not be sufficiently visible or resolvable by airborne cameras

Engineering Contradiction:
Improveland area occupiedVSAvoidmarker visibility and resolution
Core Design Contradiction:
Area of stationary objectVSMeasurement precision

Solution Approach 1:

The invention changes the optical parameters of the location marker by using a mirror to reflect sunlight. This creates a bright, high-contrast reference point that is highly visible to airborne cameras despite the mirror's small physical size. The reflected sunlight provides sufficient brightness and resolution for accurate calibration without requiring large land area occupation.

Inventive Principle:
Principle #35Parameter changes

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 precise calibration of satellite imaging systems with compact markers that reduce land occupancy and eliminate the need for satellite maneuvers, allowing for accurate determination of spatial coordinates and feature locations in images.

Implementation Method 1

A compact, mobile location marker system using a mirror capable of tilting about orthogonal axes to track the sun and reflect its beam towards the satellite

Methodology Applied
Scientific EffectReflection: Reflection

Data Source

PatentUS7768631B1Method and system for providing a known reference point for an airborne imaging platform
Publication Date: 2010.08.03 ISRAEL AEROSPACE IND LTD
  • US7768631B1 patent drawing
  • US7768631B1 patent drawing
  • US7768631B1 patent drawing

AI summary

Method for providing a known reference point for an airborne imaging system, the method including providing at measured earth co-ordinates a camera/mirror assembly having a camera and a mirror mounted in fixed mutual spatial relationship and capable of tilting about two mutually orthogonal axes. Using the camera to track the sun and produce at least two or more different measured times respective time tagged camera images. Using the time tagged camera images to obtain a transformation of mirror axes relative to axes of the earth at a mirror location on the earth where the mirror is mounted.During a time window when the mirror is within a line of sight of the airborne imaging system and the sun, adjusting the azimuth and elevation of the mirror so that the sun is reflected by the mirror toward the airborne imaging system thereby capturing an image of the mirror in an aerial image produced by the airborne imaging system. Determining a location in the aerial image corresponding to the mirror thus providing a known earth reference location in said aerial image.