Aircraft Emitter Verification via Physical Layer Signal Analysis

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Solution Overview

Problem

Current air traffic control systems lack direct identification of aircraft generating radiofrequency signals, and existing ADS-B systems are vulnerable to spoofing, posing safety concerns due to the lack of encryption and easy manipulation of aircraft location data.

Innovation Solution

A method and system that measure physical and data content features of ADS-B signals to verify their origin from an aircraft, using Gaussian mixture models and voice recognition engines to identify the emitter and distinguish between real and spoofed signals, integrating with air traffic control displays for real-time identification.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If ADS-B broadcasts are transmitted without encryption, then the system is simple to implement and decode, but the system becomes vulnerable to spoofing and security risks

Engineering Contradiction:
Improveease of implementationVSAvoidsecurity against spoofing
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent changes the physical layer parameters of the signal by introducing PN spreading sequences and encryption algorithms. This transforms the original unencrypted ADS-B signal into an encrypted form that maintains compatibility with existing receivers while adding security. The parameter change from clear text to encrypted signal resolves the contradiction by making spoofing difficult without compromising the basic ADS-B functionality.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent introduces an intermediary encryption layer between the ADS-B message generation and transmission. This intermediary component (the encryption module with PN spreading) acts as a mediator that protects the original message while allowing legitimate receivers to decrypt and process it. This resolves the security vulnerability without eliminating the ease of implementation for authorized users.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If physical layer feature measurement is added to verify signal origin, then identification accuracy improves, but system complexity increases

Engineering Contradiction:
Improvesignal origin identification accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent applies preliminary action by pre-calculating and storing the expected physical layer features (such as PN spreading sequences, encryption keys, and signal characteristics) in a database before signal verification. When a signal is received, the system simply compares the measured features against the pre-stored reference data. This approach improves identification accuracy while minimizing the complexity of real-time processing.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system employs self-service by having aircraft automatically generate and transmit their own physical layer features along with the ADS-B messages. The aircraft's transponder includes the encrypted signal and associated verification data, eliminating the need for external calibration or manual configuration. This self-service mechanism improves measurement precision without adding significant complexity to the overall system.

Inventive Principle:
Principle #25Self-service

3Reliability

If encryption and PN spreading are applied to ADS-B broadcasts, then security against spoofing improves, but signal decoding complexity increases

Engineering Contradiction:
Improvesecurity against spoofingVSAvoiddecoding complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent applies partial action by implementing encryption and PN spreading only on specific critical fields of the ADS-B message rather than the entire signal. The most important identification and location data are encrypted with PN spreading, while less critical information remains in clear text or uses simpler protection. This selective approach improves security against spoofing while keeping decoding complexity manageable for receivers.

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS9917657B1Verification of aircraft emitter
Publication Date: 2018.03.13 ROCKWELL COLLINS INC
  • US9917657B1 patent drawing
  • US9917657B1 patent drawing
  • US9917657B1 patent drawing

AI summary

A method and system. The method includes receiving at least one signal and measuring at least one physical layer feature of the at least one signal. The method further includes determining that the at least one signal originated from an emitter of an aircraft based on the at least one measured physical layer feature of the at least one signal.