Aircraft Intent Processor Residual Calculation

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Solution Overview

Problem

Current air traffic management systems face challenges in accurately predicting aircraft trajectories, which limits capacity and safety in congested airspace, and fails to accommodate operator-preferred routes and environmental considerations.

Innovation Solution

An aircraft intent processor that calculates residual data to compare actual aircraft states with intended states, enabling better correspondence between predicted and actual trajectories, and facilitating more accurate trajectory predictions and control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If current air traffic management systems use standard routes (STAR/SID) for aircraft, then safety and separation are maintained, but trajectory prediction accuracy and operator preference accommodation are limited

Engineering Contradiction:
Improvetrajectory prediction accuracyVSAvoidoperator preference accommodation
Core Design Contradiction:
Measurement precisionVSAdaptability or versatility

Solution Approach 1:

The system continuously compares predicted aircraft trajectories with actual trajectories and uses this feedback to improve prediction accuracy. The trajectory prediction module receives actual aircraft state data and adjusts predictions based on the difference between predicted and actual positions, enabling more accurate forecasting while accommodating operator-preferred routes.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system transitions from fixed standard route parameters to dynamic trajectory parameters that can be continuously adjusted. By representing aircraft intent as flexible four-dimensional trajectories (position, velocity, attitude, weight over time) rather than rigid standard routes, the system achieves both accurate prediction and accommodation of operator preferences through parameter optimization.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If air traffic management increases aircraft separation to maintain safety, then safety is preserved, but air traffic capacity and throughput are reduced

Engineering Contradiction:
Improveair traffic capacityVSAvoidsafety separation
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system replaces the mechanical constraint of fixed standard routes with a computational trajectory prediction and optimization system. By using advanced algorithms to predict and adjust aircraft trajectories in real-time, the system can maintain smaller separations while preserving safety, thereby increasing air traffic capacity without compromising reliability.

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

3Adaptability or versatility

If aircraft follow fixed standard routes, then trajectory predictability is improved, but environmental impact reduction and flexibility are compromised

Engineering Contradiction:
Improveroute flexibilityVSAvoidenvironmental impact
Core Design Contradiction:
Adaptability or versatilityVSObject-generated harmful factors

Solution Approach 1:

The system makes aircraft trajectories dynamic rather than static by continuously optimizing paths based on real-time conditions. The trajectory prediction module adjusts aircraft paths dynamically to minimize environmental impact (noise and emissions) while maintaining flexibility for operator preferences, replacing rigid standard routes with adaptive optimized trajectories.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS10041809B2Aircraft intent processor
Publication Date: 2018.08.07 THE BOEING CO
  • US10041809B2 patent drawing
  • US10041809B2 patent drawing
  • US10041809B2 patent drawing

AI summary

Example aircraft intent processors are described herein that can be used both for the prediction of an aircraft's trajectory from aircraft intent, and the execution of aircraft intent for controlling the aircraft. An example aircraft intent processor includes an aircraft intent input to receive aircraft intent data representative of aircraft intent instructions, an aircraft state input to receive state data representative of a state of the aircraft, and a residual output. The aircraft intent processor is to calculate residual data representative of an error between a state of the aircraft commanded by the received aircraft intent data and the state of the aircraft expressed by received state data, and output the residual data via the residual output.