Orbital Path Visualization With Synchronized Graph Views

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Solution Overview

Problem

Current visualization systems for tracking space objects, such as satellites, face challenges in effectively displaying and managing vast amounts of data, including historical and real-time orbital data, which can be overwhelming and difficult to interpret due to the high dimensionality of the data sets.

Innovation Solution

A system is developed that includes a visualization interface capable of receiving and processing real-time and historical data, using a network configuration with various modules to generate interactive graphs like longitude-time, scalar-time, and longitude-latitude graphs, allowing users to pan, zoom, and synchronize axes for better data interpretation and management.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If vast amounts of orbital data are displayed in traditional visualization systems, then data completeness is improved, but data interpretability deteriorates due to high dimensionality and overwhelming complexity

Engineering Contradiction:
Improvedata completenessVSAvoiddata interpretability
Core Design Contradiction:
Quantity of substanceVSEase of operation

Solution Approach 1:

The patent segments orbital data into multiple synchronized graph views (longitude-time, scalar-time, longitude-latitude graphs), each displaying specific parameters. This allows comprehensive data representation while organizing information into manageable, interpretable sections that users can navigate independently.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces a temporal dimension by synchronizing multiple graph views across different time points. Users can pan and zoom through time while maintaining synchronized views across different parameter spaces, transforming static high-dimensional data into an interactive temporal exploration experience.

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

2Device complexity

If traditional visualization interfaces are used for orbital data, then system simplicity is improved, but interaction capability deteriorates when handling high-dimensional data sets

Engineering Contradiction:
Improvesystem simplicityVSAvoidinteraction capability
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The patent implements a universal synchronized graph interface that handles multiple types of orbital data (longitude, latitude, scalar parameters) across multiple time points using a single consistent interaction model. Users interact with all views through the same panning, zooming, and synchronization mechanisms, providing versatility without increasing operational complexity.

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

Solution Approach 2:

The patent introduces a synchronization mechanism as an intermediary that coordinates multiple graph views. This mediator automatically adjusts display parameters across all views based on user interactions with any single view, enabling complex multi-parameter exploration through simple localized user actions.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Loss of information

If comprehensive orbital parameters are displayed simultaneously, then information completeness is improved, but visual clarity deteriorates due to data density

Engineering Contradiction:
Improveinformation completenessVSAvoidvisual clarity
Core Design Contradiction:
Loss of informationVSIllumination intensity

Solution Approach 1:

The patent divides comprehensive orbital parameters into separate synchronized graph views, each dedicated to specific parameter types (spatial coordinates, scalar values, temporal relationships). This segmentation prevents visual clutter while maintaining complete information availability across the synchronized views.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent uses the temporal dimension to separate information display across different time points while maintaining synchronization. Users can explore complete parameter sets at different moments in time, distributing information density across the time dimension rather than compressing it into a single overwhelming view.

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

Data Source

PatentUS11402986B2Systems and visualization interfaces for orbital paths and path parameters of space objects
Publication Date: 2022.08.02 EXOANALYTIC SOLUTIONS INC
  • US11402986B2 patent drawing
  • US11402986B2 patent drawing
  • US11402986B2 patent drawing

AI summary

A display system can be configured to receive, via a user interface, a first identifier associated with a first space object and determine a first maneuver of the first space object. The first maneuver can include a perturbation of the path of the first space object. Based on the first identifier and the first maneuver, the display system can identify one or more path parameters associated with a path of the first space object and generate a display interface. The display interface can include a longitude-time graph having a longitude axis spanning from a lower-longitude limit to an upper-longitude limit and a time axis spanning from the lower-time limit to the upper-time limit and an indication of the one or more path parameters.