Aircraft Flight Path Planning Using Tail-Specific Weather Modeling

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Solution Overview

Problem

Existing flight path determination systems rely on generic performance data, leading to inaccuracies and inefficiencies in fuel and time management, as they do not account for tail-specific aircraft performance and real-time weather conditions.

Innovation Solution

A system and method using a control unit with a machine learning model that utilizes tail-specific data and real-time weather conditions to simulate and determine the most efficient flight path, incorporating an artificial neural network to analyze flight data and weather information for precise fuel and time calculations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If generic performance data is used for flight path determination, then the system is simple to operate and requires minimal data input, but the accuracy of fuel and time calculations deteriorates

Engineering Contradiction:
Improvefuel and time calculation accuracyVSAvoiddata collection and processing system
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system performs preliminary data collection and processing by gathering tail-specific aircraft performance data and weather conditions before flight path determination. This advance preparation enables accurate real-time calculations without adding complexity during critical flight decision-making moments.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The control unit acts as an intermediary that processes tail-specific aircraft performance data and weather conditions, translating these complex inputs into accurate fuel and time calculations. This intermediary layer shields pilots from data complexity while delivering precise results.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If flight paths are determined statically before flight without adjustments, then the flight plan is simple to file and manage, but the system cannot adapt to changing weather conditions and operational dynamics

Engineering Contradiction:
Improveresponse to changing weather and operational conditionsVSAvoidtime for pilots to assess route changes
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The system continuously monitors weather conditions and operational parameters during flight, providing real-time feedback to the control unit. This enables dynamic flight path adjustments without requiring pilots to manually assess changing conditions, saving time while improving adaptability.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The flight path determination transitions from a static pre-flight calculation to a dynamic process that continuously adapts to changing weather and operational conditions. The control unit recalculates optimal paths in real-time, enabling the system to respond to dynamics while reducing pilot workload.

Inventive Principle:
Principle #15Dynamics

3Productivity

If air traffic controllers assume shorter routes are better without considering weather and mission profile, then route selection is quick and simple, but the overall flight efficiency and fuel consumption deteriorate

Engineering Contradiction:
Improveflight efficiencyVSAvoidflight path assessment system
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The system changes the assessment parameters from simple distance metrics to comprehensive evaluations including tail-specific performance data, weather conditions, and mission profile. This enables air traffic controllers to identify more efficient routes without manually analyzing multiple factors, improving productivity while managing complexity through automated processing.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS20260038375A1System and method for determining a flight path for an aircraft
Publication Date: 2026.02.05 THE BOEING CO
  • US20260038375A1 patent drawing
  • US20260038375A1 patent drawing
  • US20260038375A1 patent drawing

AI summary

A system and a method include an aircraft including a user interface having a display. A control unit is in communication with the user interface. The control unit is configured to determine a flight path for a flight of the aircraft based on tail-specific data for the aircraft, and weather conditions.