Aircraft Flight Path Planning Using Predicted Noise Waypoints

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Solution Overview

Problem

Aircraft noise remains a significant issue for communities near airports due to improved navigation techniques leading to increased overflight frequencies, despite regulatory efforts to control noise levels.

Innovation Solution

A method for generating aircraft flight paths that predicts noise levels at multiple waypoints and uses these predictions to optimize flight paths, reducing ground-level noise through the use of a computing system and machine learning models.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If navigation techniques are improved to increase flight efficiency, then aircraft can overfly communities with increased frequency, but ground-level noise increases

Engineering Contradiction:
Improveflight efficiencyVSAvoidground-level noise
Core Design Contradiction:
ProductivityVSObject-generated harmful factors

Solution Approach 1:

The system dynamically adjusts flight path parameters (altitude, lateral position, speed) to minimize noise impact on ground communities while maintaining flight efficiency. By changing these parameters in real-time based on predicted noise levels, the system resolves the contradiction between efficient routing and noise reduction.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The system uses predicted noise level feedback from machine learning models to continuously optimize flight paths. The noise predictions are fed back into the path planning algorithm to adjust subsequent routing decisions, creating a closed-loop system that balances efficiency and noise reduction.

Inventive Principle:
Principle #23Feedback

2Object-generated harmful factors

If flight paths are optimized to reduce noise, then community disturbance decreases, but flight path complexity increases

Engineering Contradiction:
Improvecommunity disturbanceVSAvoidflight path complexity
Core Design Contradiction:
Object-generated harmful factorsVSDevice complexity

Solution Approach 1:

The system performs preliminary noise level predictions at multiple waypoints before finalizing the flight path. By pre-calculating noise impacts and identifying optimal routing options in advance, the system reduces community disturbance without requiring complex real-time adjustments during flight.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The flight path is divided into multiple segments between waypoints, with noise optimization applied to each segment independently. This segmentation allows the system to manage complexity by breaking down the overall path optimization into smaller, more manageable decisions at each waypoint.

Inventive Principle:
Principle #1Segmentation

3Measurement precision

If noise predictions are calculated at multiple waypoints, then flight path optimization accuracy improves, but computational requirements increase

Engineering Contradiction:
Improvenoise prediction accuracyVSAvoidcomputational energy
Core Design Contradiction:
Measurement precisionVSUse of energy by stationary object

Solution Approach 1:

The system calculates noise predictions at a selected subset of critical waypoints rather than all possible points along the flight path. This partial action approach maintains sufficient prediction accuracy for effective optimization while significantly reducing the computational energy required compared to exhaustive calculations.

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS20250165007A1Aircraft flight path noise reduction
Publication Date: 2025.05.22 THE BOEING CO
  • US20250165007A1 patent drawing
  • US20250165007A1 patent drawing

AI summary

A method for aircraft flight path generation includes, at a computing system, receiving, for a plurality of waypoints in a geographic area, predicted aircraft noise levels for an aircraft at each waypoint of the plurality of waypoints, the predicted aircraft noise levels predicted based at least in part on a plurality of flight parameters for the aircraft. The predicted aircraft noise levels are input to a flight path prediction system configured to generate a candidate flight path for the aircraft through the geographic area based at least in part on the predicted aircraft noise levels. The candidate flight path is output from the flight path prediction system, wherein the candidate flight path is predicted to result in less ground-level noise when followed by the aircraft as compared to an alternate flight path through the geographic area.