Avionics Acquisition Channel Self-Test for Aging Signal Correction

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing acquisition systems for critical avionics face high development, production, and operational costs due to stringent safety standards, complexity, and limited ability to detect flaws beyond sudden failures, leading to oversized systems with increased electricity consumption, bulk, and weight.

Innovation Solution

An acquisition system that includes self-test means to analyze and correct digital signals by dynamically executing a reverse operating model, allowing for detection of normal, downgraded, or failure modes, and incorporating learning mechanisms to calibrate parameters and compensate for accuracy losses, thereby adapting to aging and reducing unnecessary oversizing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If redundant acquisition systems with lower criticality level are used to decrease costs, then manufacturing cost is reduced, but device complexity increases due to multiple voting systems

Engineering Contradiction:
Improvemanufacturing costVSAvoiddevice complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The acquisition system performs self-tests autonomously using stored reference signals and a reverse operating model to detect flaws and determine operating modes without external intervention, eliminating the need for complex external monitoring and voting systems

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system implements continuous self-testing with feedback loops that compare acquired signals against reference signals, automatically detect flaws, determine operating modes, and trigger corrective actions, creating a closed-loop system that replaces complex open-loop redundancy

Inventive Principle:
Principle #23Feedback

2Reliability

If acquisition systems are oversized in production to avoid aging, then reliability is improved, but weight and bulk increase

Engineering Contradiction:
ImprovereliabilityVSAvoidweight
Core Design Contradiction:
ReliabilityVSWeight of stationary object

Solution Approach 1:

The system dynamically adapts its operating mode based on real-time self-test results and detected aging effects, transitioning between normal, downgraded, and failure modes as needed, replacing static oversized design with dynamic adaptation

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes operational parameters based on detected aging and flaw conditions, adjusting accuracy thresholds and correction strategies to maintain reliability without requiring permanent oversizing of hardware

Inventive Principle:
Principle #35Parameter changes

3Reliability

If self-test means with reverse operating model are added to detect flaws, then reliability is improved, but device complexity increases

Engineering Contradiction:
ImprovereliabilityVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system creates a reverse operating model that copies and inverts the normal signal flow path, injecting reference signals through the acquisition channel and comparing results to detect flaws, using virtual modeling instead of physical redundancy

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The self-test means serve multiple functions: they generate reference signals, acquire test signals, compare signals to detect flaws, determine operating modes, and trigger corrections, consolidating what would otherwise require separate systems into a single multi-functional module

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

Data Source

PatentUS10317244B2System for acquisition of at least one physical variable, in particular for a critical on-board avionics system, and associated acquisition method
Publication Date: 2019.06.11 THALES SA
  • US10317244B2 patent drawing
  • US10317244B2 patent drawing
  • US10317244B2 patent drawing

AI summary

The present invention relates to a system for acquisition of at least one physical variable, in particular for a critical on-board avionics system, comprising a sensor for measuring the physical variable; an acquisition channel receiving an analog signal corresponding to the physical variable measured by the sensor and transforming this analog signal into a corresponding digital signal, at least some of these transformations being able to be carried out with loss of accuracy; self-test unit for checking the integrity of the acquisition channel and generating a self-test result. The system further comprises an analyzer analyzing the self-test result in order to determine an operating mode of the acquisition channel, and for activating the operation of means for correcting the signal delivered by the channel.