Satellite Navigation Provider Selection Using Geolocation Neural Networks

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Solution Overview

Problem

Existing methods for selecting satellite navigation service providers are complex and inflexible, requiring large databases that incur high computational costs and are difficult to update when geopolitical changes occur.

Innovation Solution

A computer-implemented method using artificial neural networks to determine the authorization of satellite navigation service providers based on geographical position, allowing for simple and flexible selection without the need for a complex database, and enabling easy adaptation to changes in provider use restrictions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If a large database is used to cover the entire surface of the earth, then the coverage is complete, but the database size becomes very large and computational cost increases

Engineering Contradiction:
Improvegeographical coverage areaVSAvoiddatabase size
Core Design Contradiction:
Area of stationary objectVSDevice complexity

Solution Approach 1:

The patent divides the geographical coverage into smaller regions by using multiple satellite constellations (GPS, GLONASS, Galileo, Beidou), each covering specific areas. This segmentation allows complete global coverage without requiring a single massive database, as each constellation maintains its own smaller position database.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent transitions from a two-dimensional geographical coverage problem to a multi-dimensional solution by incorporating multiple satellite constellations operating in different orbital planes and using different frequency bands. This dimensional expansion allows overlapping coverage areas to be managed separately, reducing the complexity of any single database.

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

2Adaptability or versatility

If the database is regenerated when provider selection changes, then the latest geopolitical restrictions are reflected, but the computational cost is very high

Engineering Contradiction:
Improveadaptability to geopolitical changesVSAvoidcomputational cost
Core Design Contradiction:
Adaptability or versatilityVSLoss of energy

Solution Approach 1:

The patent implements a dynamic provider selection mechanism where the aircraft's navigation system automatically evaluates multiple satellite constellations and selects the most appropriate one based on real-time criteria such as signal quality, availability, and geopolitical restrictions. This dynamic approach allows the system to adapt to changes without regenerating the entire database, as the selection logic can be updated independently.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent pre-establishes selection criteria and provider authorization rules in the database before flight operations. These pre-defined rules include geopolitical restrictions and service availability information. During flight, the system simply applies these pre-computed rules to the current satellite signals, avoiding the need for real-time database regeneration when restrictions change.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If basic satellite constellations are used to meet IFR requirements, then safety and reliability requirements must be reinforced, but the system complexity increases

Engineering Contradiction:
Improvesafety and reliability for IFR operationsVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent merges multiple satellite constellation systems (GPS, GLONASS, Galileo, Beidou) into a unified navigation solution. By combining these constellations, the system achieves the required safety and reliability for IFR operations through redundancy and cross-validation, while managing complexity through a standardized selection framework that treats all constellations uniformly.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The patent implements a feedback mechanism where the aircraft's navigation system continuously monitors signal quality, satellite availability, and position accuracy from multiple constellations. Based on this feedback, the system automatically adjusts provider selection to maintain IFR compliance, reinforcing reliability without requiring complex manual intervention or system reconfiguration.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS12579899B2Method for selecting at least one satellite navigation service provider and associated selection system
Publication Date: 2026.03.17 THALES SA
  • US12579899B2 patent drawing
  • US12579899B2 patent drawing
  • US12579899B2 patent drawing

AI summary

A method for selecting at least one satellite navigation service provider from a plurality of predetermined providers, the selection method being computer-implemented and comprising: a step for receiving a geographical position; a step of determining an indication relating to the authorization of use of at least one provider of the plurality of predetermined providers, the determining step being implemented by at least one artificial neural network (24) associated with said provider, an input variable of the artificial neural network (24) being the geographical position, an output variable of the artificial neural network (24) being said indication; a step for selecting at least one provider for satellite navigation of an aircraft.