Aircraft Pilot Fatigue Detection and Controlled Rest Control

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Solution Overview

Problem

Current aircraft systems lack effective methods to detect and manage pilot fatigue and incapacitation, particularly during long flights, which can lead to reduced attention and increased risk of accidents due to microsleep and deep sleep stages.

Innovation Solution

A method using sensors to track pilot biometric parameters and attention levels, allowing controlled rest periods during safe phases of flight, and implementing alerts and system controls to prevent deep sleep and ensure pilot alertness, including haptic feedback, visual indicators, and automated recovery procedures.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If continuous monitoring of pilot attention is implemented, then flight safety is improved, but pilot alertness deteriorates due to constant surveillance pressure

Engineering Contradiction:
Improveflight safetyVSAvoidpilot alertness
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system implements feedback by monitoring pilot biometric parameters (eye movements, head position, breathing patterns) and providing real-time information about pilot attention state. This allows the system to detect microsleep and fatigue without requiring constant pilot self-monitoring, thus improving safety while maintaining natural pilot alertness.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The pilot's own physiological parameters serve as the monitoring mechanism. The system uses the pilot's natural bodily functions (eye movements, breathing, head position) as indicators of attention state, eliminating the need for external intervention or conscious effort from the pilot to maintain alertness.

Inventive Principle:
Principle #25Self-service

2Duration of action of moving object

If controlled rest periods are allowed, then pilot fatigue is reduced, but flight monitoring capability deteriorates during rest

Engineering Contradiction:
Improvepilot enduranceVSAvoidflight monitoring capability
Core Design Contradiction:
Duration of action of moving objectVSReliability

Solution Approach 1:

During controlled rest periods, the system continues to monitor pilot parameters and provides feedback about the pilot's sleep state. The system can detect when the pilot is entering deep sleep stages and provide gentle wake-up signals, ensuring that the pilot remains available for critical situations while still allowing beneficial rest.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system implements periodic monitoring during rest periods, checking pilot attention state at regular intervals. This allows the pilot to rest while the system periodically verifies that the pilot remains in a safe state, balancing rest benefits with monitoring requirements.

Inventive Principle:
Principle #19Periodic action

3Reliability

If automated control systems are activated during pilot incapacitation, then flight safety is improved, but pilot autonomy deteriorates

Engineering Contradiction:
Improveflight safetyVSAvoidpilot autonomy
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The system prepares automated control protocols in advance for various incapacitation scenarios. When pilot incapacitation is detected, pre-programmed procedures are automatically activated, ensuring immediate safety response while maintaining structured pilot involvement through predefined decision frameworks.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The automated system acts as an intermediary between pilot incapacitation and full aircraft control takeover. The system provides graduated levels of assistance, starting with alerts and warnings, then progressing to automated control only when absolutely necessary, thus preserving pilot autonomy while ensuring safety.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentEP3667458B1Aircraft and method of controlling
Publication Date: 2022.10.05 GE AVIATION SYST LTD
  • EP3667458B1 patent drawingFigure 1
  • EP3667458B1 patent drawingFigure 2
  • EP3667458B1 patent drawingFigure 3

AI summary

A method (140, 150) of controlling an aircraft (10) includes tracking (141, 151), using at least one sensor (103, 105, 106, 112, 117), one of an input by a pilot or a biometric parameter of a pilot during flight of the aircraft (10). The method (140, 150) also includes determining (142, 152) a lack of attention by the pilot or a depth of sleep of the pilot based on the biometric parameter.