Autopilot Approach Mode Monitoring for Missed Pilot Arming

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Solution Overview

Problem

Aircraft incidents during approach and landing are frequently caused by pilot errors, inadequate adherence to standard operating procedures, and incorrect activation of the approach mode in the autopilot system, which can lead to unstable landings and safety risks.

Innovation Solution

The system implements additional safety nets by monitoring pilot responses and automatically arming the approach mode if the pilot fails to do so within a specified time frame after the aircraft converges to the final approach path, using a combination of location data from navigation systems, timers, and alerts to ensure timely activation of the approach mode.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the approach mode is manually armed by the pilot, then the pilot maintains control and awareness of the system, but the risk of pilot error and failure to timely arm the approach mode increases

Engineering Contradiction:
Improveapproach mode activation reliabilityVSAvoidpilot operation complexity
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system monitors its own operational state and automatically arms the approach mode when conditions are met, eliminating the need for continuous pilot intervention. The autopilot system self-monitors flight parameters and self-activates the approach mode, reducing reliance on pilot action while maintaining system reliability.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system continuously monitors flight conditions and provides feedback to determine when approach mode arming is appropriate. By monitoring flight path convergence and other parameters, the system uses feedback loops to automatically trigger approach mode arming when conditions are satisfied, ensuring timely activation without pilot error.

Inventive Principle:
Principle #23Feedback

2Reliability

If the approach mode is automatically armed when conditions are met, then the risk of pilot error is reduced, but the system complexity increases

Engineering Contradiction:
Improveapproach mode activation reliabilityVSAvoidautopilot system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The existing autopilot system's flight mode controller is enhanced to perform multiple functions: it continues to manage normal flight mode transitions while also monitoring approach conditions and automatically arming approach mode. This multi-functionality reduces the need for separate dedicated systems while improving reliability.

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

Solution Approach 2:

The system performs preliminary monitoring of flight conditions and automatically arms approach mode in advance when conditions are met, before the pilot would need to manually arm it. This preliminary automatic action ensures the approach mode is ready when needed, reducing the need for complex real-time pilot decisions.

Inventive Principle:
Principle #10Preliminary action

3Loss of information

If the system provides multiple alerts before automatic arming, then pilot awareness is improved, but the time required for pilot response increases

Engineering Contradiction:
Improvepilot awareness of approach mode statusVSAvoidtime to arm approach mode
Core Design Contradiction:
Loss of informationVSLoss of time

Solution Approach 1:

The system uses periodic alerting with a timer that provides alerts at predetermined intervals before automatic arming occurs. This periodic notification system ensures the pilot is aware of the approach mode status and has multiple opportunities to manually arm it, while the structured timing prevents excessive delays.

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The system provides preliminary alerts to the pilot before automatic arming occurs, giving advance notice and opportunity for manual intervention. These preliminary actions inform the pilot of the approaching automatic arming event, maintaining awareness while establishing a clear timeline for response.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11586196B2Approach mode activation monitoring function and automatic activation in an event of pilot incapacitation
Publication Date: 2023.02.21 HONEYWELL INTERNATIONAL INC
  • US11586196B2 patent drawing
  • US11586196B2 patent drawing
  • US11586196B2 patent drawing

AI summary

Aircraft systems and methods that determine, based on location data from a navigation system, whether conditions have been met enabling arming of an approach mode of an autopilot system. The systems and methods, when the one or more conditions enabling arming of the approach mode are determined to be met, start a first timer of a first period of time and, at the same time, provide a first message to alert a pilot to arm the approach mode via manual input to a user interface. When a determination has been made that the approach mode continues to have not been armed via manual input to the user interface, the approach mode is automatically armed.