Flight Management Decision Point Detection for Trajectory Rejoining

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Solution Overview

Problem

Current flight management systems fail to accurately predict transit times and manage constraints when an aircraft deviates from its planned trajectory, leading to errors in rejoining the flight plan and uncertainty for pilots regarding compliance with altitude, speed, and time constraints.

Innovation Solution

A method for determining decision points on a shifted aircraft trajectory where the aircraft can no longer rejoin a constrained waypoint, using predefined criteria such as rejoining angles, aircraft speed, and thrust parameters to guide the rejoining process, allowing for optimal or limit rejoining based on predefined constraints.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If the flight management system assumes immediate return to flight plan after controller instruction, then calculation complexity is reduced, but transit time prediction accuracy deteriorates

Engineering Contradiction:
Improvecalculation complexityVSAvoidtransit time prediction accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The system pre-calculates and stores rejoining trajectories and decision points before they are needed. When a controller instruction is received, the system retrieves pre-computed information about where and how the aircraft can rejoin the flight plan, avoiding complex real-time calculations while maintaining accurate transit time predictions.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system dynamically adjusts the rejoining strategy based on current flight conditions. It calculates decision points that consider the aircraft's current position, speed, and the specific controller instruction being followed, allowing the transit time predictions to adapt to the actual dynamic situation rather than assuming a fixed immediate return.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If the pilot follows controller instructions deviating from flight plan, then operational flexibility is improved, but compliance with flight plan constraints deteriorates

Engineering Contradiction:
Improveoperational flexibilityVSAvoidcompliance with flight plan constraints
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The system continuously monitors the aircraft's position and calculates decision points that provide feedback to the pilot about when to initiate rejoining maneuvers. This feedback mechanism ensures that even when following controller instructions, the pilot receives guidance on maintaining eventual compliance with flight plan constraints through timely rejoining actions.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system pre-calculates decision points and rejoining trajectories before the pilot needs to make a decision. By providing this information in advance, the system enables the pilot to follow controller instructions with confidence knowing that compliance with flight plan constraints can be achieved by initiating rejoining at the predetermined decision points.

Inventive Principle:
Principle #10Preliminary action

3Adaptability or versatility

If the flight management system calculates rejoining trajectories in real-time, then adaptability to current conditions is improved, but calculation time and processing load increase

Engineering Contradiction:
Improveadaptability to current conditionsVSAvoidcalculation time
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The system pre-calculates rejoining trajectories and decision points based on various possible flight conditions and stores them for quick retrieval. This preliminary action eliminates the need for complex real-time calculations while maintaining adaptability, as the pre-computed data can be quickly matched to current flight conditions.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system calculates and stores more rejoining trajectories than strictly necessary, covering a range of possible flight conditions. This excessive pre-calculation ensures that the system has pre-computed solutions ready for any situation that may arise, reducing real-time processing requirements while maintaining high adaptability.

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS9530321B2Flight management method and system
Publication Date: 2016.12.27 THALES SA
  • US9530321B2 patent drawing
  • US9530321B2 patent drawing
  • US9530321B2 patent drawing

AI summary

A method and system, for flight management of an aircraft flying on a trajectory shifted with respect to a flight plan comprising a plurality of constrained waypoints, comprises a step of determining and displaying at least one point of the trajectory, termed decision point, beyond which the aircraft can no longer rejoin a constrained waypoint of the flight plan by determining a point of intersection between the trajectory and a rejoining trajectory steering towards the selected constrained waypoint, the rejoining trajectory complying with at least one predefined criterion.