Encrypted Navigation Signals for Secure LEO Satellite Positioning

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing satellite navigation systems face challenges in providing secure, precise, and efficient location and time transfer services, as well as accurate atmospheric and environmental monitoring, particularly in low earth orbit (LEO) scenarios, due to limitations in data transmission and processing capabilities.

Innovation Solution

A satellite constellation system comprising LEO satellites equipped with navigation processing systems that utilize encrypted navigation messages, radio occultation, and inter-satellite communication to provide secure precision location and time transfer services, atmospheric monitoring, and environmental data, leveraging atomic clocks and edge computing for enhanced data processing and control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If higher power navigation signals are transmitted from LEO satellites, then navigation precision and atmospheric monitoring capability are improved, but energy consumption and satellite power system complexity increase

Engineering Contradiction:
Improvenavigation precisionVSAvoidenergy consumption
Core Design Contradiction:
Measurement precisionVSUse of energy by moving object

Solution Approach 1:

The patent changes the transmission power parameter dynamically based on operational requirements. LEO satellites adjust their signal power levels to provide higher power when precision navigation and atmospheric monitoring are needed, while reducing power during normal operations to conserve energy. This parameter adaptation resolves the contradiction by allowing high precision only when necessary.

Inventive Principle:
Principle #35Parameter changes

2Speed

If LEO satellites are used for navigation and atmospheric monitoring, then signal convergence speed and atmospheric penetration are improved, but orbital geometry limitations and coverage area reduce

Engineering Contradiction:
Improvesignal convergence speedVSAvoidcoverage area
Core Design Contradiction:
SpeedVSArea of stationary object

Solution Approach 1:

The patent divides the coverage area into multiple zones and uses a constellation of LEO satellites in different orbital planes and altitudes. Each satellite covers a specific region, and together they provide global coverage. This segmentation allows individual satellites to maintain fast signal convergence while the network as a whole achieves comprehensive area coverage.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent utilizes three-dimensional orbital geometry by deploying satellites at different altitudes and inclinations. This multi-layered spatial arrangement allows signals to reach deeper into the atmosphere for monitoring purposes while maintaining coverage over large surface areas through the combined effect of multiple satellites viewed from different dimensional perspectives.

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

3Reliability

If encryption is applied to navigation signals, then security and anti-spoofing capability are improved, but signal processing complexity and receiver computation requirements increase

Engineering Contradiction:
ImprovesecurityVSAvoidsignal processing complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent introduces cryptographic keys and authentication protocols as intermediary elements between the satellite transmitter and receiver. These intermediaries enable secure signal verification and anti-spoofing capabilities without requiring complex processing of the navigation signal itself. The encryption layer operates separately from the core navigation signal processing, maintaining reliability while managing complexity.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS12618984B2Transmitting secure navigation signals via applying encryption
Publication Date: 2026.05.05 XONA SPACE SYSTEMS INC
  • US12618984B2 patent drawing
  • US12618984B2 patent drawing
  • US12618984B2 patent drawing

AI summary

A satellite is operable to generate a navigation message. Encrypted navigation message data is generated from the navigation message by applying an encryption scheme to the navigation message. An encrypted ranging signal is generated by applying the encryption scheme to a spreading code of the satellite. A secure navigation signal is generated based on modulating the encrypted navigation message data upon the encrypted ranging signal. The secure navigation signal is broadcast for receipt by at least one client device. The secure navigation signal facilitates the at least one client device to determine state data of the at least one client device by utilizing key data associated with the encryption scheme.