Acoustic Aircraft Tracking via Distributed Sensor Network

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Solution Overview

Problem

Current aircraft tracking systems, particularly at airports, face limitations in tracking aircraft at low altitudes and in adverse environmental conditions due to the complexity and expense of ground tracking radars, and the limitations of human visual observation and electro-optical sensors, which are often obstructed or ineffective in low-visibility situations.

Innovation Solution

A distributed network of acoustic sensors around an airfield, combined with beamforming algorithms, collects and processes acoustic signatures to determine the range and bearing of aircraft, providing effective tracking capabilities even at low altitudes and in various environmental conditions, and can be integrated with existing control tower assets for comprehensive tracking.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If ground tracking radars are used to track aircraft, then tracking capability is improved, but system complexity and cost increase significantly

Engineering Contradiction:
Improvetracking capabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system divides the airfield into multiple zones with distributed acoustic sensors positioned at strategic locations. Each sensor node independently monitors its local area and transmits data to a central processing system, replacing the monolithic radar system with a modular sensor network that achieves comprehensive coverage through segmentation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent replaces the electromagnetic radar system with an acoustic detection system that uses microphones and signal processing to track aircraft. This substitution uses acoustic wave propagation and beamforming algorithms instead of electromagnetic radiation, providing effective low-altitude tracking without the complexity and cost of traditional radar infrastructure.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If ground tracking radars are used to track aircraft, then tracking capability is improved, but implementation cost increases significantly

Engineering Contradiction:
Improvetracking capabilityVSAvoidimplementation cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The system employs relatively inexpensive acoustic sensors (microphones) rather than costly radar transmitters and receivers. These acoustic sensor nodes can be deployed at low cost and replaced or repositioned as needed, providing an economical solution for airports with limited budgets while maintaining effective aircraft tracking capability.

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

Solution Approach 2:

The acoustic sensor network serves multiple functions including aircraft detection, tracking, identification, and monitoring of low-altitude flight paths. The same sensor infrastructure can be integrated with existing air traffic control systems and used for various aviation safety applications, maximizing the value of the investment through multi-functionality.

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

3Reliability

If visual observation or electro-optical sensors are used to track aircraft, then tracking capability is maintained, but effectiveness decreases in low-visibility conditions

Engineering Contradiction:
Improvetracking capabilityVSAvoidenvironmental adaptability
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The patent replaces optical detection methods with acoustic detection that is insensitive to visual conditions. Acoustic waves propagate independently of light, allowing the system to effectively track aircraft in darkness, fog, rain, or snow where optical sensors fail, providing all-weather operational capability.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

4Reliability

If electro-optical sensors are used to track aircraft, then tracking capability is provided, but effectiveness decreases due to physical obstructions

Engineering Contradiction:
Improvetracking capabilityVSAvoidphysical obstruction
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The system positions acoustic sensors at multiple strategic locations around the airfield, including elevated positions and areas with clear acoustic paths. Each sensor is optimized for its specific location and coverage area, creating a network that collectively overcomes individual obstruction limitations through distributed spatial coverage.

Inventive Principle:
Principle #3Local quality

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system enables precise localization and real-time tracking of aircraft, effectively addressing the limitations of existing methods by providing a reliable and cost-effective solution for tracking in all environmental conditions, including low altitudes and adverse weather.

Implementation Method 1

a plurality of nodes are positioned throughout an airfield and are able to observe and 'listen' for acoustical signatures of nearby aircraft

Methodology Applied
Scientific EffectAcoustic wave propagation: Sound

Implementation Method 2

beamforming algorithms on audio signals emitted by objects to track the objects

Methodology Applied
Scientific EffectBeamforming:

Data Source

PatentUS9632171B1Acoustic aircraft tracker and warning system
Publication Date: 2017.04.25 BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC
  • US9632171B1 patent drawing
  • US9632171B1 patent drawing
  • US9632171B1 patent drawing

AI summary

A system and method for tracking aircraft, helicopters and/or other objects at an airfield using acoustics of the aircraft, helicopters and/or other objects. A method receives first acoustical data at a first sensor and second acoustical data is also received at a second sensor. The first and second sensors may be carried by a first structurally supportive body member. Based at least in part on the first acoustical data and the second acoustical data a range and a bearing of the aircraft is determined from a predetermined location at the airfield. The range and bearing can be determined by using a beam forming algorithm. Based on the range and the bearing, the method displays the location the aircraft on a display.