Predicted Flight Path Depiction in Head-Up Displays

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Solution Overview

Problem

Current head-up displays and synthetic vision systems only depict the aircraft's trajectory at the current time, failing to provide a predicted flight path over a period, which limits situational awareness and decision-making capabilities for pilots.

Innovation Solution

A head-up display and synthetic vision system that includes a predicted flight path generation component, graphic generation component, and sensors to calculate and display a three-dimensional predicted flight path based on state parameters and flight dynamics equations, combining this information with a visual exterior view to project a graphical representation of the aircraft's trajectory over time.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If current head-up displays and synthetic vision systems only depict the aircraft's trajectory at the current time, then the system complexity is reduced, but situational awareness and decision-making capabilities are limited

Engineering Contradiction:
Improvesituational awarenessVSAvoidsystem complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The system performs preliminary calculation of the predicted flight path by integrating flight dynamics equations and aircraft state parameters to project future trajectory points before they occur. This allows the display to show anticipated position, velocity, and acceleration states in advance, giving pilots ahead-of-time information for decision-making without requiring complex real-time computation during critical moments

Inventive Principle:
Principle #10Preliminary action

2Loss of information

If a predicted flight path over a period is displayed, then situational awareness is enhanced, but the device complexity increases

Engineering Contradiction:
Improvetrajectory informationVSAvoiddisplay system complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The system transitions from displaying only two-dimensional current position data to incorporating a time dimension by showing multiple predicted trajectory points extending into the future. This dimensional expansion provides pilots with temporal context about the aircraft's projected path while maintaining a coherent spatial representation that integrates seamlessly with existing head-up display formats

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

3Measurement precision

If three-dimensional transforms are used to generate graphical display, then the visual representation accuracy is improved, but computational requirements increase

Engineering Contradiction:
Improvevisual representation accuracyVSAvoidcomputational power
Core Design Contradiction:
Measurement precisionVSPower

Solution Approach 1:

The predicted flight path is segmented into discrete future time points (e.g., 2 seconds, 4 seconds, 6 seconds ahead) rather than computing continuous trajectory data. At each segmented time point, three-dimensional transforms are applied to calculate position, velocity, and acceleration independently, reducing overall computational load while maintaining visual accuracy through strategically selected key moments in the predicted path

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS8963742B1Head-up display/synthetic vision system predicted flight path depiction
Publication Date: 2015.02.24 ROCKWELL COLLINS INC
  • US8963742B1 patent drawing
  • US8963742B1 patent drawing
  • US8963742B1 patent drawing

AI summary

A head-up display system includes an aircraft, a predicted flight path generation component that calculates a predicted flight path over a period of time, and a graphic generation component configured to generate a graphical display and project it onto a combiner configured to combine the graphical display with a visual exterior view. A synthetic vision system includes an aircraft, a predicted flight path generation component that receives one or more state parameters and calculates a predicted flight path over a period of time, and a synthetic terrain generation component configured to generate a synthetic view which is displayed on a display. The graphical display and/or the synthetic view includes a three-dimensional depiction of the predicted flight path over the period of time generated utilizing one or more three-dimensional transforms, one or more graphical images based on flight data, and a three-dimensional graphical depiction of a flight plan.