Orbital Visualization Interface for Space Object Tracking

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Solution Overview

Problem

Existing visualization systems for tracking orbital objects lack features and efficiency in portraying complex data, such as path parameters, maneuvers, and orbital trajectories, making it difficult to accurately analyze and predict the movements of space objects.

Innovation Solution

A system that includes a display interface configured to receive user input for identifying path parameters of space objects, generating a longitude-time graph, and displaying indications of path parameters, allowing for interactive visualization and analysis of orbital data.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If traditional visualization systems are used to track orbital objects, then basic tracking functionality is provided, but the system lacks features for effectively portraying complex path parameters and maneuvers

Engineering Contradiction:
Improvevisualization featuresVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The visualization system is designed to perform multiple functions including displaying orbital trajectories, path parameters, maneuvers, and space object identifiers within a unified interface. The system can portray various types of data (photographs, tracking data, path parameters) and support different visualization modes, making it versatile for comprehensive orbital object analysis without requiring separate specialized systems for each function

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Measurement precision

If more path parameters and orbital data are displayed, then analysis accuracy improves, but the interface becomes more complex and harder to operate

Engineering Contradiction:
Improveorbital data accuracyVSAvoidinterface usability
Core Design Contradiction:
Measurement precisionVSEase of operation

Solution Approach 1:

The complex orbital data is segmented into distinct visual components including orbital trajectories, path parameters, maneuvers, and space object identifiers. Each parameter type is displayed in a structured format with clear visual separation, allowing users to access detailed orbital information while maintaining interface clarity through organized presentation of segmented data elements

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system transforms complex multi-dimensional orbital data into visual representations on two-dimensional graphs and displays. Orbital trajectories are plotted on longitude-time graphs, path parameters are displayed with visual indicators, and maneuvers are shown as distinct markers, converting abstract numerical data into intuitive visual forms that improve accuracy without overwhelming the interface

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

3Productivity

If comprehensive orbital tracking data is collected and displayed, then tracking efficiency improves, but data processing and visualization time increases

Engineering Contradiction:
Improvetracking efficiencyVSAvoiddata processing time
Core Design Contradiction:
ProductivityVSLoss of time

Solution Approach 1:

The system performs preliminary processing and organization of orbital tracking data before full visualization is required. Data from multiple photographs and tracking sources is pre-processed to extract path parameters, identify maneuvers, and calculate orbital trajectories in advance, so that when visualization is needed, the data is already structured and ready for immediate display, reducing processing time while maintaining comprehensive tracking efficiency

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20250191135A1Systems for software-defined telescopes
Publication Date: 2025.06.12 EXOANALYTIC SOLUTIONS INC
  • US20250191135A1 patent drawing
  • US20250191135A1 patent drawing
  • US20250191135A1 patent drawing

AI summary

A system can use a plurality of co-located telescopes to generate enhanced telescopic imagery of space objects. The system may be configured to receive telescopic imagery data of a plurality of space objects obtained from the plurality of co-located telescopes. The system can receive at least two imaging criteria. The available imaging criteria can include a target signal sensitivity comprising a minimum signal to noise ratio (SNR), a target number of spectral bands comprising a minimum number of spectral bands, a spectral range associated with one or more of the spectral bands, a location of the plurality of co-located telescopes, a target data cadence comprising a minimum number of frames per minute, a target number of space objects to be tracked, a target minimum spatial resolution, among others. The system can transmit instructions to the plurality of telescopes and generate enhanced telescopic imagery.