Flight Path Management for Moving Targets

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Solution Overview

Problem

Current aircraft flight path determination methods are inefficient for navigating around moving targets, such as ships or weather systems, as they lack the ability to dynamically adjust flight paths to maintain a safe distance and optimize travel time.

Innovation Solution

A computer-implemented method and system that identifies parameters of a moving target, determines a moving circular flight path, and calculates an optimum flight path for an aircraft to intercept this path, allowing the aircraft to maintain a safe distance and reduce travel time by dynamically adjusting to the target's motion.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the aircraft flies around a moving target to maintain a safe distance, then the safety is improved, but the flight path complexity and travel time increase

Engineering Contradiction:
ImprovesafetyVSAvoidtravel time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent applies dynamics by making the flight path adaptive and movable rather than static. The circular flight path moves with the target, and the system dynamically recalculates intercept points and flight paths as the target moves, allowing the aircraft to maintain safe distance while optimizing travel time to the moving circular path

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system performs preliminary calculations of the intercept point and flight path to the moving circular flight path before the aircraft actually reaches the target area. By predicting future positions and calculating optimal paths in advance, the system reduces actual travel time while maintaining safety

Inventive Principle:
Principle #10Preliminary action

2Reliability

If the aircraft maintains a fixed distance from the moving target, then the safety is improved, but the flight path cannot be optimized for time and fuel efficiency

Engineering Contradiction:
ImprovesafetyVSAvoidfuel efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system dynamically adjusts the flight path based on the target's motion. The circular flight path moves with the target, and the intercept point is continuously recalculated, allowing the aircraft to maintain safety while optimizing for fuel efficiency through dynamic path adjustment rather than fixed distance maintenance

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes parameters such as the radius of the circular flight path, the intercept point location, and the flight path trajectory based on target motion parameters. By adjusting these parameters dynamically, the system achieves both safety and fuel efficiency

Inventive Principle:
Principle #35Parameter changes

3Measurement precision

If the system calculates a flight path to a moving circular flight path, then the accuracy and predictability are improved, but the computational complexity increases

Engineering Contradiction:
Improvedistance prediction accuracyVSAvoidcomputational complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system performs preliminary calculations of the intercept point and flight path to the moving circular flight path before the aircraft actually reaches the target area. By predicting future positions and calculating optimal paths in advance, the system achieves high accuracy while managing computational complexity through advance planning

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system uses feedback from target motion parameters to continuously update and recalculate the flight path. The circular flight path moves with the target, and the system recalculates intercept points based on updated target position and velocity, maintaining accuracy through continuous feedback adjustment

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS10242578B2Flight path management system
Publication Date: 2019.03.26 GE AVIATION SYSTEMS LLC
  • US10242578B2 patent drawing
  • US10242578B2 patent drawing
  • US10242578B2 patent drawing

AI summary

Systems and methods for determining a flight path of an aircraft are provided. In one embodiment, a method can include identifying one or more parameter(s) associated with a moving target. The method can include determining a moving circular flight path associated with the moving target based at least in part on the parameter(s) associated with the moving target. The method can include identifying one or more condition(s) associated with at least one of the aircraft and the moving circular flight path. The method can include determining a flight path of the aircraft from a location of the aircraft to the moving circular flight path based at least in part on the parameter(s) associated with the moving target and the condition(s) associated with at least one of the aircraft and the moving circular flight path.