Flight Management System External Plan Validation

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Solution Overview

Problem

The integration of external flight plan changes with flight management systems poses challenges due to potential discrepancies in data interpretation by avionics systems, leading to increased pilot workload and error risks, as pilots must review external data before transferring it to avionics, but existing solutions fail to efficiently validate these changes.

Innovation Solution

A system that coordinates with the flight management system on-board an aircraft to validate flight plan changes generated by external devices by receiving aircraft state and weather data, generating deviations, and displaying graphical user interface overlays to indicate changes, allowing pilots to select and confirm valid travel paths that meet savings parameters.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If external flight plan changes are transmitted to the flight management system, then flight plan updates are achieved, but data discrepancies and pilot workload increase

Engineering Contradiction:
Improveflight plan update efficiencyVSAvoiddata interpretation accuracy
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system performs preliminary validation of external flight plan changes by comparing them against the flight management system's own flight plan data before transmission. This preliminary action identifies discrepancies early, preventing invalid data from reaching the avionics system and reducing pilot workload.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system acts as an intermediary between external flight plan sources and the flight management system. It receives external flight plan changes, validates them against FMS data, and only transmits validated changes to the avionics system, thereby ensuring data accuracy and reducing pilot burden.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If pilots review external flight plan data before transfer, then data accuracy is maintained, but pilot workload increases

Engineering Contradiction:
Improvedata transfer accuracyVSAvoidpilot workload
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system performs self-validation by automatically comparing external flight plan changes against the FMS flight plan data without requiring pilot intervention. This automated self-service maintains data accuracy while eliminating the manual review workload for pilots.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The manual mechanical review process performed by pilots is replaced with an automated electronic validation system that compares flight plan data programmatically. This substitution maintains accuracy while significantly reducing pilot workload.

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

3Adaptability or versatility

If multiple connectivity features are integrated, then system capability is enhanced, but pilot complexity and error risk increase

Engineering Contradiction:
Improveconnectivity feature capabilityVSAvoidpilot operational complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The validation process is segmented into distinct automated steps: receiving external flight plan changes, comparing against FMS data, identifying discrepancies, and transmitting only validated changes. This segmentation manages complexity by breaking down the multifaceted connectivity challenge into manageable automated tasks.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS12125393B2Systems and methods to corroborate an externally recommended flight plan change with flight management system
Publication Date: 2024.10.22 HONEYWELL INTERNATIONAL INC
  • US12125393B2 patent drawing
  • US12125393B2 patent drawing
  • US12125393B2 patent drawing

AI summary

Systems and methods for coordinating with a flight management system (FMS) on-board an aircraft to determine whether a flight plan (FP) change generated by an external device is valid. The method includes generating the FP change, which includes a deviation to the intended FP and a savings parameter associated with a parameter of the intended FP, responsive to weather data and aircraft state data; generating a lateral display showing the intended FP and an alphanumeric window with the FP change; transmitting the FP change to the FMS; receiving, from the FMS, a travel path and a calculated parameter for the travel path, generated by the FMS responsive to the FP change; determining whether the travel path realizes the savings parameter by comparing the calculated parameter to the savings parameter; and, displaying either a selectable graphical user interface (GUI) object to implement the FP change, or a warning based thereon.