Satellite ADS-B Beam Scheduling for Global Aircraft Monitoring

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Solution Overview

Problem

Conventional radar-based air traffic control and aircraft surveillance systems are limited to regions with ground infrastructure, leaving vast areas unmonitored, and while terrestrial ADS-B systems are being adopted, they also face similar coverage gaps.

Innovation Solution

Implementing a space-based ADS-B system with satellites equipped with receivers and antennas to receive and relay ADS-B messages, utilizing reconfigurable FPGAs for processing and beam adjustment, and a ground segment for routing messages to destinations, enabling global coverage.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If conventional radar-based air traffic control systems are used, then aircraft surveillance is achievable, but coverage is limited to regions with ground infrastructure

Engineering Contradiction:
Improvecoverage areaVSAvoidsystem complexity
Core Design Contradiction:
Area of stationary objectVSDevice complexity

Solution Approach 1:

The patent transitions from ground-based radar systems operating in two dimensions (horizontal coverage) to space-based satellite systems operating in three dimensions (global coverage including oceans and remote areas). This dimensional shift enables monitoring of previously inaccessible regions without proportionally increasing system complexity.

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

Solution Approach 2:

The satellite-based ADS-B receiver system performs multiple functions: receiving ADS-B messages from aircraft, processing position information, and relaying data to ground segments. This multi-functional approach consolidates surveillance capabilities into a single platform, expanding coverage area while managing system complexity through integration.

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

2Reliability

If terrestrial ADS-B systems are deployed, then air traffic monitoring capability is improved, but coverage gaps remain in areas without ground infrastructure

Engineering Contradiction:
Improvemonitoring capabilityVSAvoidcoverage area
Core Design Contradiction:
ReliabilityVSArea of stationary object

Solution Approach 1:

The invention moves the monitoring function from terrestrial ground stations to orbiting satellites, enabling coverage of oceanic and remote terrestrial regions that are inaccessible to ground-based systems. This spatial repositioning maintains reliable ADS-B reception while eliminating coverage gaps.

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

Solution Approach 2:

The satellite acts as an intermediary between aircraft and ground infrastructure, receiving ADS-B messages directly from aircraft transponders and relaying position information to ground segments. This intermediary approach enables monitoring in areas where direct ground-based reception is impossible.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Area of stationary object

If space-based ADS-B system is implemented, then global coverage is achieved, but system complexity increases

Engineering Contradiction:
Improvecoverage areaVSAvoidsystem complexity
Core Design Contradiction:
Area of stationary objectVSDevice complexity

Solution Approach 1:

The system is divided into distinct functional segments: satellite-based ADS-B receivers in orbit, space segment for signal processing, and ground segment for data routing. This segmentation allows global coverage through distributed satellites while managing complexity by localizing processing functions to autonomous satellite units with standardized interfaces.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent employs reconfigurable FPGAs that can dynamically adjust reception parameters such as beam direction and frequency tuning based on satellite position and traffic patterns. This parameter adaptability enables a single satellite design to maintain effective coverage across varying orbital positions and operational conditions, reducing the need for multiple specialized systems.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS20250386276A1Space-based aircraft monitoring
Publication Date: 2025.12.18 AIREON LLC
  • US20250386276A1 patent drawing
  • US20250386276A1 patent drawing
  • US20250386276A1 patent drawing

AI summary

In one implementation, a system for space-based aircraft monitoring includes a ground segment, multiple aircraft monitoring payloads on board corresponding satellites, and a resource scheduling system. Individual payloads include antenna systems configured to provide multiple beams for receiving ADS-B messages and two or more receivers configured to process received ADS-B messages that are implemented, at least in part, by reconfigurable FPGAs. In addition, individual payloads are configured to initiate transmission of ADS-B messages processed by one or more of their receivers to the ground segment. Meanwhile, the ground segment is configured to receive such messages and to route them to one or more destinations for aircraft monitoring. The resource scheduling system is configured to control the antenna systems of individual payloads to dynamically adjust the beams for receiving ADS-B messages of the individual antenna systems.