Virtual ADS-B IN for Aircraft Situational Awareness in Oceanic Airspace

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Solution Overview

Problem

Aircraft lacking ADS-B IN capability often lack situational awareness within an airspace, leading to inefficient flight paths and reduced fuel efficiency, especially in non-surveillance areas like oceanic regions, and existing systems like ITP and PTM require costly installations and re-certification.

Innovation Solution

A system providing virtual ADS-B IN capability through a tracking sub-system with an ADS-B receiver that determines situational information from ADS-B OUT signals, allowing aircraft without ADS-B receivers to receive situational signals for improved flight planning and control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If aircraft without ADS-B IN capability follow traditional surveillance procedures, then they can operate in non-surveillance airspace, but they lack situational awareness and must fly at non-optimal flight levels reducing fuel efficiency

Engineering Contradiction:
Improvesituational awarenessVSAvoidfuel efficiency
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The patent introduces an intermediary system (ground-based tracking system with ADS-B receiver) that mediates between aircraft without ADS-B IN capability and the surrounding airspace traffic. The system receives ADS-B OUT signals from other aircraft, processes this information, and provides situational awareness data back to aircraft without ADS-B IN capability, enabling them to make informed flight level decisions while maintaining fuel efficiency.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If aircraft install ADS-B receivers to gain situational awareness, then they can receive information from other aircraft, but installation is costly and requires re-certification

Engineering Contradiction:
Improvesituational awarenessVSAvoidinstallation cost and complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent creates a virtual copy of ADS-B IN capability for aircraft that do not physically possess it. By implementing a ground-based tracking system that receives ADS-B OUT signals and replicates this information back to aircraft without receivers, the system provides the functional equivalent of ADS-B IN capability without requiring actual installation of receivers on the aircraft, thereby avoiding installation costs and re-certification requirements.

Inventive Principle:
Principle #26Copying

3Reliability

If air traffic control uses large procedural separation standards in non-surveillance airspace, then safety is maintained, but the number of aircraft that can fly simultaneously is limited

Engineering Contradiction:
ImprovesafetyVSAvoidairspace density
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent implements a feedback mechanism where the ground-based tracking system continuously monitors ADS-B OUT signals from aircraft and provides real-time situational awareness information back to aircraft without ADS-B IN capability. This feedback loop enables more precise separation decisions based on actual aircraft positions and trajectories rather than relying solely on fixed procedural separation standards, thereby increasing airspace density while maintaining safety.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS12548451B2Systems and methods for improving situational awareness of aircraft within an airspace
Publication Date: 2026.02.10 THE BOEING CO
  • US12548451B2 patent drawing
  • US12548451B2 patent drawing
  • US12548451B2 patent drawing

AI summary

A system and a method include a control unit configured to determine situational information regarding a plurality of aircraft within an airspace. The control unit is configured to determine the situational information based on automatic dependent surveillance-broadcast (ADS-B) signals output by the plurality of aircraft and received by an ADS-B receiver of a tracking sub-system.