ADS-B Multilateration for UAV Location Accuracy

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Solution Overview

Problem

Compact aircraft systems, such as unmanned aircraft systems (UAS), face challenges in determining their location accurately due to design restrictions and resource limitations, as they often cannot support Global Navigation Satellite System (GNSS) hardware, and existing multilateration techniques require multiple satellite-based signals.

Innovation Solution

A system that uses directional or omnidirectional antennas to receive secondary surveillance radar (SSR) signals from at least four proximate non-satellite objects, processing these signals to determine the ownship location using multilateration and position metrics, such as accuracy data from Automatic Dependent Surveillance-Broadcast (ADS-B) signals, without relying on satellite-based navigation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If GNSS-based hardware is used for positioning, then location accuracy is improved, but size, weight, power consumption, and cost increase

Engineering Contradiction:
Improvelocation accuracyVSAvoidsystem weight
Core Design Contradiction:
Measurement precisionVSWeight of moving object

Solution Approach 1:

The patent uses ADS-B signals from other aircraft as an intermediary means to determine position. Instead of directly using GNSS hardware, the system receives position information from nearby aircraft that are broadcasting their GPS-derived locations, thereby obtaining positioning capability without carrying heavy GNSS equipment.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system copies position information from other aircraft's ADS-B transmissions. By receiving and processing the broadcast position data from multiple aircraft, the system reconstructs its own position indirectly through multilateration, using copied data rather than direct satellite measurement.

Inventive Principle:
Principle #26Copying

2Measurement precision

If GNSS-based hardware is used for positioning, then location accuracy is improved, but device complexity increases

Engineering Contradiction:
Improvelocation accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent extracts only the necessary positioning function from the complex GNSS system. By receiving ADS-B signals that already contain processed position information from other aircraft, the system extracts positioning capability without implementing the entire GNSS receiver chain, reducing complexity while maintaining accuracy.

Inventive Principle:
Principle #2Taking out (Extraction)

3Measurement precision

If multiple satellite-based signals are used for multilateration, then location determination accuracy is improved, but the system becomes incompatible with compact aircraft designs

Engineering Contradiction:
Improvelocation determination accuracyVSAvoidsystem compatibility
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

Instead of using satellite-based signals as the primary positioning source, the patent inverts the approach by using ground-based or air-based ADS-B transmitters (other aircraft) as the positioning sources. The receiving aircraft determines its position by measuring signals from these non-satellite sources, reversing the traditional satellite-to-ground signal flow.

Inventive Principle:
Principle #13The other way round (Inversion)

Data Source

PatentUS10244364B1System and method for location determination using received ADS-B accuracy data
Publication Date: 2019.03.26 UAVIONIX CORP
  • US10244364B1 patent drawing
  • US10244364B1 patent drawing
  • US10244364B1 patent drawing

AI summary

A system and related methods for location determination aboard a subject vehicle not equipped with a GNSS-based positioning system receives position signals transmitted by non-satellite atmospheric vehicles and surface objects, which may include precise locations of the transmitting objects or position metrics associated with containment regions within which the transmitting objects should be to a particular certainty level. The received position signals may include ADS-B signals transmitted by proximate aircraft and facilities. The system may determine ownship location via multilateration of received position signals, via processing the received position metrics and corresponding containment regions, or via combining or correlating the two to determine accurate ownship location data of the subject vehicle.