Formal Language Aircraft Intent Prediction

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Solution Overview

Problem

Current air traffic management systems lack the accuracy and commonality needed to predict aircraft trajectories unambiguously, leading to inefficiencies in air traffic handling and potential safety issues due to varying trajectory modeling approaches and limited coordination between ground and airborne systems.

Innovation Solution

A computer-implemented method using a formal language to express aircraft intent, which involves receiving and storing flight information, deriving instructions for aerodynamic configuration and motion, and ensuring compliance with rules to provide a common framework for aircraft intent description, enabling accurate and synchronized trajectory predictions across different systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If different trajectory modeling approaches are used by ground and airborne systems, then system flexibility is maintained, but prediction accuracy and commonality deteriorate

Engineering Contradiction:
Improvesystem flexibilityVSAvoidprediction accuracy
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The patent applies universality by creating a common trajectory modeling framework that can be used by both ground-based ATM systems and airborne Flight Management Systems. The standardized intent description language and formal semantics enable different systems to use the same modeling approach, ensuring prediction accuracy and commonality while maintaining the flexibility to express diverse flight intents through a unified interface.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Adaptability or versatility

If flight intent is used as a basic blueprint, then operational flexibility is maintained, but trajectory unambiguity deteriorates

Engineering Contradiction:
Improveoperational flexibilityVSAvoidtrajectory unambiguity
Core Design Contradiction:
Adaptability or versatilityVSLoss of information

Solution Approach 1:

The patent introduces an intermediary layer between the flexible flight intent blueprint and the specific trajectory computation. The formal intent description language with standardized semantics acts as a mediator that translates operational flexibility into unambiguous trajectory specifications, ensuring that the basic blueprint can be interpreted consistently across different systems and contexts.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent applies parameter changes by transforming the qualitative flight intent parameters into quantitative, standardized parameters in the formal description language. This transformation process converts flexible operational concepts into precise, unambiguous specifications that can be reliably processed by trajectory computation systems while preserving the original operational intent.

Inventive Principle:
Principle #35Parameter changes

3Ease of operation

If aircraft intent is expressed without a formal language, then ease of communication is maintained, but prediction reliability deteriorates

Engineering Contradiction:
Improveease of communicationVSAvoidprediction reliability
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The patent replaces informal, natural language communication about aircraft intent with a formalized description language. This substitution transforms subjective, ambiguous expressions into objective, precisely-defined specifications that can be reliably processed by computational systems, thereby maintaining ease of communication through standardized interfaces while dramatically improving prediction reliability.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS9250099B2Predicting aircraft trajectory
Publication Date: 2016.02.02 THE BOEING CO
  • US9250099B2 patent drawing
  • US9250099B2 patent drawing
  • US9250099B2 patent drawing

AI summary

The present invention provides a computer-implemented method of producing a description of aircraft intent expressed using a formal language. The description may be used to predict aircraft trajectory, for example by air traffic management. Rules are used in association with information provided to generate a set of instructions describing both the aerodynamic configuration of the aircraft and the motion of the aircraft. These instructions are checked to ensure that they describe unambiguously the aircraft's trajectory. The instructions are then expressed using a formal language.