Flight Management System Altitude Time Fix Generation

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Solution Overview

Problem

Existing aircraft Flight Management Systems (FMS) lack features to determine coordinates for altitude or time targets relative to an aircraft's trajectory, limiting navigation and control capabilities.

Innovation Solution

The system receives target values for altitude or time, calculates the corresponding aircraft position, and displays the distance to travel to reach that position, providing coordinates for integration into the flight management system to modify flight plans and improve navigation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If existing FMS fix info functions are used, then basic navigation capabilities are maintained, but the system lacks features to determine coordinates for altitude or time targets relative to aircraft trajectory

Engineering Contradiction:
Improvenavigation capabilityVSAvoidfix coordinates
Core Design Contradiction:
Adaptability or versatilityVSLoss of information

Solution Approach 1:

The system pre-calculates and stores fix coordinates for various altitude and time targets along the aircraft's trajectory before they are needed for navigation decisions, allowing the FMS to quickly provide accurate position information without real-time computation delays

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent introduces an intermediary calculation layer between the flight management system and the navigation display, which computes intermediate fix points based on altitude and time parameters, then provides these calculated coordinates to the user interface for navigation planning

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If the FMS calculates and displays target aircraft position and distance, then navigation accuracy is improved, but the system complexity increases

Engineering Contradiction:
Improveposition accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The FMS is enhanced to perform multiple functions using the same core calculation engine: it can compute fix coordinates for altitude targets, time targets, or a combination of both, and can provide this information in different formats (coordinates, distance, time estimates) without requiring separate dedicated systems for each function

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

Solution Approach 2:

The flight management system automatically calculates and updates fix coordinates based on the current flight plan and aircraft performance data, without requiring manual intervention or external computational resources, making the enhanced functionality self-sufficient

Inventive Principle:
Principle #25Self-service

3Productivity

If the system provides comprehensive fix information including coordinates and distance, then flight management efficiency is improved, but the ease of operation may be reduced due to additional information processing

Engineering Contradiction:
Improveflight management efficiencyVSAvoiduser interface complexity
Core Design Contradiction:
ProductivityVSEase of operation

Solution Approach 1:

The user interface presents different levels of information detail in different contexts: basic navigation displays show only essential fix points, while detailed navigation planning modes provide comprehensive coordinate and distance information, allowing users to access full functionality when needed without being overwhelmed during routine operations

Inventive Principle:
Principle #3Local quality

Data Source

PatentUS20240428694A1Generating time and altitude based fixes for a flight management system
Publication Date: 2024.12.26 THE BOEING CO
  • US20240428694A1 patent drawing
  • US20240428694A1 patent drawing
  • US20240428694A1 patent drawing

AI summary

Techniques for aircraft flight management are disclosed. These techniques include receiving, at a flight management system (FMS) of an aircraft, a target value, the target value including at least one of: (i) an altitude target value or (ii) a time target value. The techniques further include determining a target aircraft position relating to the target value, based on a trajectory for the aircraft. The techniques further include calculating a distance for the aircraft to travel from a current aircraft position to the target aircraft position and displaying the calculated distance in a user interface of the aircraft. The techniques further include providing coordinates for the target aircraft position to the FMS for use in flight management of the aircraft.