Airspace Information Model Dynamic Design Optimization

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Solution Overview

Problem

Current airspace design and planning tools are static and non-responsive to dynamic changes in air traffic demand, leading to inefficient operations, increased fuel consumption, noise, and emissions, as they fail to account for the interdependencies between various operational systems involved in airspace management.

Innovation Solution

The Airspace Information Model (AIM) integrates design, performance evaluation, and optimization into a single system, using a holistic approach that includes a parametric model, user interface, and simulation functions to provide real-time feedback and evaluation of Key Performance Indicators (KPIs) such as fuel burn, noise levels, and emissions, enabling dynamic airspace design and planning.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If static airspace design is used, then system complexity is reduced, but air traffic demand responsiveness deteriorates

Engineering Contradiction:
Improveairspace design system complexityVSAvoidairspace responsiveness to air traffic demand
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The airspace design system transitions from static to dynamic by continuously updating airspace configurations based on real-time air traffic demand data. The system dynamically adjusts airspace parameters such as route positions, altitude assignments, and sector boundaries to respond to changing traffic patterns, thereby resolving the contradiction between system complexity and adaptability.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system implements feedback mechanisms by monitoring air traffic demand in real-time and using this information to continuously optimize airspace design. The feedback loop enables the system to automatically adjust airspace configurations based on observed traffic patterns, resolving the contradiction by making the system adaptive without requiring excessive complexity.

Inventive Principle:
Principle #23Feedback

2Area of stationary object

If longer flight distances are required, then airspace coverage is improved, but fuel consumption increases

Engineering Contradiction:
Improveairspace coverage areaVSAvoidfuel consumption
Core Design Contradiction:
Area of stationary objectVSUse of energy by moving object

Solution Approach 1:

The system changes flight path parameters dynamically by optimizing route positions, waypoints, and altitude assignments based on real-time conditions. This allows aircraft to reach the same airspace coverage areas through more efficient paths, reducing flight distances and fuel consumption while maintaining comprehensive airspace coverage.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The system utilizes the vertical dimension by optimizing altitude assignments and three-dimensional flight paths. Instead of only horizontal route adjustments, the system can assign different altitudes to various flight segments, enabling more direct and fuel-efficient routes that maintain adequate airspace coverage through vertical separation and routing optimization.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Measurement precision

If more comprehensive modeling is performed, then evaluation accuracy is improved, but computational time increases

Engineering Contradiction:
Improveperformance evaluation accuracyVSAvoidcomputational time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The system performs preliminary actions by pre-calculating and storing performance evaluation criteria, design rules, and validation parameters before actual airspace design operations. This preparation enables faster real-time evaluations without sacrificing accuracy, as the computational framework is already established and ready for rapid application to specific design scenarios.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The comprehensive modeling is segmented into modular components, each handling specific aspects of performance evaluation and validation. This segmentation allows the system to process evaluations in discrete, manageable steps rather than as a single computationally intensive operation, reducing overall computational time while maintaining comprehensive and accurate assessment of airspace designs.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS11783711B2Airspace information modeling and design
Publication Date: 2023.10.10 VIANAIR INC
  • US11783711B2 patent drawing
  • US11783711B2 patent drawing
  • US11783711B2 patent drawing

AI summary

Methods and systems for efficient airspace design and planning using the Airspace Information Model are described. In one example aspect, a method for designing an improved airspace model includes receiving a first user input that comprises one or more parameters, generating, based on the first user input, an airspace design, performing a validation of the airspace design against an aviation standard, the validation comprising a set of design rules and criteria for evaluation of aircraft performance and safety of operations, generating, based on at least the parametric model, at least one key performance indicator (KPI) for the airspace design, providing for display a value of the at least one KPI, receiving a second user input that comprises an updated value for at least one of the one or more parameters, and providing for display, based on the second input, an updated value of the at least one KPI.