High Frequency Sensor Data Integration for Aircraft Anomaly Detection

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Solution Overview

Problem

Current Integrated Vehicle Health Management systems are inadequate in processing and analyzing high-frequency sensor data, leading to inefficiencies in diagnosing equipment failures and degradation in complex systems like vehicles, and are costly to maintain due to high false alarm rates and the need for frequent software and hardware upgrades.

Innovation Solution

A method that integrates high-frequency sensor data with low-frequency sensor data using a Model-Based Reasoner engine, which processes and analyzes sensor information from various sources, including high-frequency sensors, to identify anomalies and provide real-time diagnostic analysis, reducing false alarms and maintenance costs by using a physics-based approach and XML model configuration.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If high-frequency sensor data is processed and integrated with low-frequency sensor data, then diagnostic accuracy and system reliability are improved, but device complexity and processing requirements increase

Engineering Contradiction:
Improvediagnostic accuracyVSAvoidprocessing complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent segments sensor data processing by frequency characteristics, separating high-frequency sensor data processing from low-frequency sensor data processing. This allows the system to handle different data types with appropriate methods, improving diagnostic accuracy while managing complexity through modular architecture.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent adds a frequency dimension to sensor data processing, organizing data along the frequency spectrum rather than treating all sensor data uniformly. This dimensional organization enables more efficient processing and integration of diverse sensor inputs, balancing reliability improvement with complexity management.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Ease of manufacture

If rules-based diagnostic approaches are used, then implementation is simple, but false alarm rates increase and effectiveness decreases

Engineering Contradiction:
Improveimplementation simplicityVSAvoiddiagnostic effectiveness
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent replaces traditional rules-based diagnostic approaches with a model-based reasoning system that uses physics-based models and mathematical relationships. This substitution improves diagnostic effectiveness and reduces false alarms by using fundamental physical principles rather than empirical rules, while maintaining implementation feasibility through structured modeling approaches.

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

3Loss of energy

If traditional sensor processing methods are used, then processing cost is low, but high-frequency sensor data cannot be adequately handled

Engineering Contradiction:
Improveprocessing costVSAvoidhigh-frequency data handling capability
Core Design Contradiction:
Loss of energyVSAdaptability or versatility

Solution Approach 1:

The patent introduces dynamic processing capabilities that adapt to the frequency characteristics of sensor data. The system dynamically adjusts processing methods based on whether data is high-frequency or low-frequency, enabling adequate handling of high-frequency data while managing processing costs through selective application of appropriate processing techniques.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS10725463B1High frequency sensor data analysis and integration with low frequency sensor data used for parametric data modeling for model based reasoners
Publication Date: 2020.07.28 NORTHROP GRUMMAN SYSTEMS CORP
  • US10725463B1 patent drawing
  • US10725463B1 patent drawing
  • US10725463B1 patent drawing

AI summary

A method implemented by a computing system identifies anomalies that represents potential off-normal behavior of components on an aircraft based on data from sensors during various modes of operations including in-flight operation of the aircraft. High-frequency sensor outputs monitor performance parameters of respective components. Anomaly criteria is dynamically selected and the high-frequency sensor outputs are compared with the anomaly criteria where the comparison results determine whether potentially off-normal behavior exists. A conditional anomaly tag is inserted in the digitized representations of first high-frequency sensor outputs where the corresponding comparison results indicate potentially off-normal behavior. At least the digitized representations of the first high-frequency sensor outputs containing the conditional anomaly tag are sent to a computer-based diagnostic system for a final determination of whether the conditional anomaly tag associated with the respective components represents off-normal behavior for the respective components.