Synchronous Scrambler Offset Estimation Under Linear Error Coding

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Solution Overview

Problem

Existing technologies face challenges in efficiently and quickly detecting the initial state of a synchronous scrambler in unmanned aircraft systems (UAS) due to the presence of linear error control codes and noise, which is crucial for drone detection and mitigation systems.

Innovation Solution

A method involving nulling the linear error control code, obtaining a system of equations, and using a min-sum procedure to recover the initial state of the synchronous scrambler, which includes performing soft nulling on the linear error control code and using a min-sum procedure to decode the scrambler state.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If linear error control code is used for encoding, then reliability of transmission is improved, but difficulty of detecting and measuring the initial scrambler state increases

Engineering Contradiction:
Improvetransmission reliabilityVSAvoiddifficulty of detecting initial scrambler state
Core Design Contradiction:
ReliabilityVSDifficulty of detecting and measuring

Solution Approach 1:

The patent extracts and removes the linear error control code component from the received signal through nulling operations. By applying the null space matrix of the error control code to the received vector, the method separates and eliminates the code component, allowing the underlying scrambler state to be detected without interference from the error control encoding.

Inventive Principle:
Principle #2Taking out (Extraction)

2Object-affected harmful factors

If synchronous scrambler is used for encryption, then security is improved, but ease of operation for detection and mitigation decreases

Engineering Contradiction:
Improvesecurity against drone threatsVSAvoidease of detection and mitigation
Core Design Contradiction:
Object-affected harmful factorsVSEase of operation

Solution Approach 1:

The patent performs preliminary nulling of the linear error control code before attempting to detect the scrambler state. This preparatory step simplifies the subsequent detection process by removing the complicating factor of error control encoding, making the overall detection and mitigation operation easier while maintaining security.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent introduces a null space matrix as an intermediary tool to facilitate the detection process. This matrix acts as a mediator that transforms the received signal by eliminating the error control code component, enabling easier extraction of scrambler state information without compromising the security provided by the synchronous scrambler.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If noise is present in the received signal, then reliability of detection decreases, but the need for robust detection methods increases

Engineering Contradiction:
Improvedetection reliabilityVSAvoidnoise interference
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent extracts and removes the structured linear error control code component from the noisy received signal. By applying nulling operations with the null space matrix, the method separates the code component from the noise and scrambler state, allowing for more reliable detection of the initial scrambler state despite the presence of noise.

Inventive Principle:
Principle #2Taking out (Extraction)

Data Source

PatentUS20250385817A1Systems and methods for estimating offset of synchronous scramblers
Publication Date: 2025.12.18 SKYSAFE INC
  • US20250385817A1 patent drawing
  • US20250385817A1 patent drawing
  • US20250385817A1 patent drawing

AI summary

Systems and methos for estimating offset of synchronous scramblers are provided. In one aspect, a method of estimating an initial state of a synchronous scrambler in the presence of a linear error control code includes receiving a vector including a transmit bit vector encoded using the linear error control code, and performing nulling on the linear error control code to null impact of the linear error control code from the received vector. The method also includes obtaining a system of equations from the received vector in response to performing the nulling on the linear error control code, and using a min-sum procedure to recover the initial state of the synchronous scrambler from the system of equations.