Orbital Path Visualization With Synchronized Multi-Graph Analysis
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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 large datasets, generating interactive displays with synchronized graphs (longitude-time, scalar-time, and longitude-latitude) that allow users to pan, zoom, and interact with the data, enabling the identification of path parameters and maneuvers of space objects, and providing tools for data integration and user settings to customize the display.
Engineering Contradictions & Design Principles
Engineering 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
Solution Approach 1:
The system segments orbital data into multiple synchronized graph views (longitude-time, scalar-time, longitude-latitude) that can be independently explored. Each graph displays specific parameters separately, allowing users to analyze different aspects of orbital data without being overwhelmed by all dimensions simultaneously, thus maintaining data completeness while improving interpretability.
Solution Approach 2:
The system transforms high-dimensional orbital data into multi-dimensional visual space by creating synchronized graph views that map different parameters across separate axes and views. This dimensional transformation allows complex orbital parameters to be visualized in an extended visual space, making the data more interpretable without losing information.
2Loss of information
If multiple orbital parameters are displayed simultaneously, then information completeness is improved, but visualization complexity deteriorates
Solution Approach 1:
The synchronized graph system provides multi-functionality by displaying multiple orbital parameters across different graph views that all share a common time axis. Each graph can display different parameters (longitude, scalar, latitude) while maintaining synchronization, allowing comprehensive information display without creating a single overly complex visualization.
Solution Approach 2:
The system segments different orbital parameters into separate graph views (longitude-time, scalar-time, longitude-latitude), where each graph focuses on specific parameters. This segmentation reduces the visual complexity of individual graphs while maintaining information completeness through the collection of synchronized views.
3Measurement precision
If detailed orbital data is presented, then analysis precision is improved, but user accessibility deteriorates
Solution Approach 1:
The system provides dynamic interaction capabilities where users can pan, zoom, and explore orbital data at different levels of detail. Users can start with an overview view for accessibility and then zoom into specific time periods or parameters for detailed analysis, making the system adaptable to different user needs and expertise levels.
Solution Approach 2:
The system adds temporal dimension through synchronized time axes across multiple graphs, allowing users to precisely analyze orbital parameters over time while maintaining contextual understanding. The multi-view approach provides both detailed precision and contextual accessibility simultaneously.
Data Source
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.