Space Object Tracker Combining Imaging and LIDAR Ranging

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Solution Overview

Problem

Conventional ground-mounted facilities are inefficient in tracking space objects, particularly small-sized resident space objects, due to atmospheric interference and limited detection capabilities, leading to incomplete information retrieval and impaired mission planning.

Innovation Solution

An object tracker equipped with an imaging unit and a light detection and ranging (LIDAR) unit that captures images and emits laser beams to determine attributes of space objects, including a transmitter, receiver, and processing circuitry to accurately track and measure angular position and range.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If ground mounted facilities are used to track space objects, then infrastructure simplicity is maintained, but detection capability deteriorates due to atmospheric interference

Engineering Contradiction:
Improveinfrastructure simplicityVSAvoiddetection capability
Core Design Contradiction:
Ease of manufactureVSMeasurement precision

Solution Approach 1:

The patent transitions from ground-based tracking to space-based tracking by deploying the tracking facility in orbit. This dimensional change from Earth's surface to space eliminates atmospheric interference, enabling detection of small-sized RSOs that are invisible from ground level while maintaining operational simplicity through standardized satellite platform integration.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Duration of action of stationary object

If ground mounted facilities operate during rainfall or snowfall, then continuous monitoring is attempted, but sensor performance deteriorates due to atmospheric conditions

Engineering Contradiction:
Improvecontinuous monitoringVSAvoidsensor performance
Core Design Contradiction:
Duration of action of stationary objectVSReliability

Solution Approach 1:

The patent extracts the tracking facility from the Earth's atmosphere by deploying it in space. This removal eliminates the harmful atmospheric conditions (rainfall, snowfall) that degrade ground-based sensor performance, ensuring continuous and reliable monitoring regardless of weather conditions on Earth.

Inventive Principle:
Principle #2Taking out (Extraction)

3Device complexity

If imaging unit alone is used to detect RSO attributes, then system complexity is minimized, but information completeness deteriorates due to limited detection capabilities

Engineering Contradiction:
Improvesystem complexityVSAvoidinformation completeness
Core Design Contradiction:
Device complexityVSLoss of information

Solution Approach 1:

The patent merges two complementary detection systems: an imaging unit for capturing visual information and determining angular position, and a LIDAR unit for measuring range through laser time-of-flight. This combination provides complete three-dimensional positioning information (angular position + range) that neither system could achieve alone, significantly improving information completeness.

Inventive Principle:
Principle #5Merging (Combining)

4Use of energy by stationary object

If ground mounted facilities track space objects, then operational cost is reduced, but tracking coverage deteriorates to only 4% of lethal space objects

Engineering Contradiction:
Improveoperational costVSAvoidtracking coverage
Core Design Contradiction:
Use of energy by stationary objectVSQuantity of substance

Solution Approach 1:

The patent employs multiple space-based tracking facilities deployed in different orbital positions to achieve comprehensive global coverage. This multi-platform approach in space enables tracking of all lethal RSOs regardless of their orbital characteristics, in contrast to the limited 4% coverage achievable from ground level.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

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

The object tracker effectively tracks small-sized space objects, providing comprehensive information for improved space mission planning and operational capabilities in various environmental conditions.

Implementation Method 1

The imaging unit is configured to capture one or more images of space around the object tracker to search for a resident space object (RSO) in the space

Methodology Applied
Scientific EffectOptical radiation detection: Light

Implementation Method 2

the LIDAR unit is coupled to the imaging unit and configured to activate upon receipt of the first set of attributes from the imaging unit such that the LIDAR unit emits, based on the first set of attributes, a laser beam towards the RSO to determine a second set of attributes of the RSO

Methodology Applied
Scientific EffectLIDAR (Light Detection and Ranging): LIDAR

Implementation Method 3

The receiver is configured to receive reflected version of the laser beam upon striking of the laser beam with the RSO. The photodetector, based on the laser beam and the reflected version of the laser beam, determines the second set of attributes

Methodology Applied
Scientific EffectPhotodetection: Photoelectric Effect

Data Source

PatentUS20250341638A1Object tracker and method thereof
Publication Date: 2025.11.06 DIGANTARA IND PTE LTD
  • US20250341638A1 patent drawing
  • US20250341638A1 patent drawing
  • US20250341638A1 patent drawing

AI summary

Disclosed is an object tracker (106) having an imaging unit (202) and a light detection and ranging (LIDAR) unit (204). The imaging unit (202) is configured to capture one or more images of space around the object tracker (106) to search for a resident space object (RSO) (102a) in the space. Upon detection of the RSO (102a), the imaging unit (202) determines a first set of attributes of the RSO (102a). The LIDAR unit 204 is configured to activate upon receipt of the first set of attributes from the imaging unit (202) such that the LIDAR unit (204) emits, based on the first set of attributes, a laser beam towards the RSO (102a) to determine a second set of attributes of the RSO (102a).