Flight Plan Micro-Shortcuts With ATC-Approved RNAV 5 Routing

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Solution Overview

Problem

Existing flight plans often require aircraft to adhere to strict navigation corridors, limiting the implementation of shortcuts that could conserve fuel, especially in densely populated areas where air traffic control may not allow deviations.

Innovation Solution

An aircraft system that modifies flight plans to implement micro-shortcuts within RNAV 5 boundaries by identifying suitable segments, obtaining air traffic control permission, and calculating the shortest path within geographical environments, using a flight plan modification algorithm integrated with the flight management system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the aircraft follows the strict navigation corridor (RNAV 5 boundaries), then the aircraft adheres to air traffic control regulations, but the flight distance increases and fuel consumption increases

Engineering Contradiction:
Improveadherence to air traffic control regulationsVSAvoidfuel consumption
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The flight plan is divided into multiple segments between waypoints, and the system evaluates each segment individually to determine if a micro-shortcut can be implemented. This segmentation allows the aircraft to follow strict corridors where necessary while exploiting opportunities for fuel-saving shortcuts in suitable areas, thus resolving the contradiction between regulatory adherence and fuel efficiency.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Instead of applying shortcuts across the entire flight plan, the system implements micro-shortcuts partially - only in segments where conditions permit (clear airspace, approved by ATC, within RNAV 5 boundaries). This partial application maintains regulatory compliance in critical areas while achieving fuel savings in permissible zones.

Inventive Principle:
Principle #16Partial or excessive action

2Loss of energy

If the aircraft implements shortcuts outside RNAV 5 boundaries, then the flight distance decreases and fuel consumption decreases, but the aircraft violates air traffic control regulations

Engineering Contradiction:
Improvefuel consumptionVSAvoidadherence to air traffic control regulations
Core Design Contradiction:
Loss of energyVSReliability

Solution Approach 1:

The system changes the parameter of corridor width dynamically - using the full RNAV 5 boundary allowance (5 nautical miles either side) when implementing micro-shortcuts, rather than strictly following the centerline. This parameter adjustment enables shorter flight paths while remaining within regulatory limits.

Inventive Principle:
Principle #35Parameter changes

3Loss of energy

If the aircraft requests deviation permission from air traffic control, then the aircraft may implement shortcuts, but the communication time and operational complexity increase

Engineering Contradiction:
Improvefuel consumptionVSAvoidoperational complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The system performs preliminary evaluation of potential micro-shortcut segments before flight, identifying suitable candidates where shortcuts can be implemented without requiring complex real-time ATC coordination. This advance preparation reduces operational complexity during actual flight while still enabling fuel-saving maneuvers.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP3882891B1Systems and methods for flight plan modifications
Publication Date: 2025.07.16 HONEYWELL INTERNATIONAL INC
  • EP3882891B1 patent drawingFigure 1
  • EP3882891B1 patent drawingFigure 2
  • EP3882891B1 patent drawingFigure 3

AI summary

Methods and systems for modifying a flight plan to implement micro-shortcuts. The system identifies a segment of interest within an initial flight plan, the segment of interest being a section to consider for a micro-shortcut. The system determined a geographical environment associated with the segment of interest and determines a relevant air traffic control (ATC) for the geographical environment. The system requests, from the relevant ATC, an amount of deviation from the initial flight plan for the segment of interest. Upon obtaining permission for the amount of deviation from the initial flight plan for the segment of interest, the system calculates a shortest path (i.e., a micro-shortcut) for the segment of interest. The system modifies the initial flight plan and commands the FMS to fly the shortest path for the segment of interest.