Flight Path Input via Touchscreen Trace and Constraint Validation

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Solution Overview

Problem

Current flight management systems require pilots to input flight paths as data points, which can be cumbersome and lack a user-friendly interface for quickly modifying routes based on additional data such as terrain and weather, potentially leading to unattainable flight paths.

Innovation Solution

A method that involves receiving a trace input of a selected flight path on a touch screen or cursor control device, generating a final flight path considering aircraft performance attributes, and displaying it on the flight deck, while adapting the path to account for geographic and weather constraints to ensure it is attainable.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If pilots input flight paths as data points in traditional FMS, then the system can process the input, but the interface becomes cumbersome and time-consuming

Engineering Contradiction:
Improveinterface usabilityVSAvoidtime to input flight path
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The patent replaces the traditional mechanical data-point input method with a graphical touch-screen interface where pilots can directly draw or select flight paths visually. This substitution of input mechanism dramatically improves ease of operation and reduces the time required to input flight path information.

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

Solution Approach 2:

The system allows pilots to copy or replicate flight path segments by selecting and dragging existing path elements, rather than manually entering each data point. This copying mechanism accelerates the flight path input process while maintaining accuracy.

Inventive Principle:
Principle #26Copying

2Productivity

If pilots manually input flight paths without system validation, then input is quick, but the flight path may be unattainable due to terrain or weather constraints

Engineering Contradiction:
Improveflight path creation speedVSAvoidflight path attainability
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system performs preliminary validation of the flight path against terrain, weather, and aircraft performance constraints before finalizing the route. This preliminary check ensures that the quickly created flight path is attainable and safe, resolving the contradiction between speed and reliability.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system provides immediate feedback to the pilot when a drawn flight path violates constraints such as terrain clearance or weather avoidance requirements. This feedback loop allows the pilot to quickly adjust the path while maintaining both speed of creation and attainability.

Inventive Principle:
Principle #23Feedback

3Reliability

If the system provides detailed terrain and weather data processing, then flight path safety improves, but system complexity increases

Engineering Contradiction:
Improveflight path safetyVSAvoidsystem processing complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system automatically performs terrain and weather constraint analysis without requiring manual configuration or complex pilot intervention. The FMS self-services by integrating these data processing functions directly into the flight path creation workflow, maintaining safety while managing complexity through automation.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS8797190B2Method for displaying a user entered flight path
Publication Date: 2014.08.05 GE AVIATION SYSTEMS LLC
  • US8797190B2 patent drawing
  • US8797190B2 patent drawing
  • US8797190B2 patent drawing

AI summary

A method for selecting and displaying a flight path for an aircraft on a display of a flight deck of the aircraft that allows a user to input a selected flight path on a map displayed on the display. A final flight path will be displayed on the display of the flight deck that is based on the input of the selected flight path.