Aircraft Display System for Smooth 3D to 2D Perspective Transition

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current aircraft flight information display systems experience a harmful loss of reference for pilots during abrupt transitions between three-dimensional and two-dimensional perspectives, disrupting the pilot's situational awareness and decision-making process.

Innovation Solution

A system that generates and displays successive three-dimensional transition synthesis images, centered around an intermediate central point of interest, with varying observation distance and opening angle as functions of the transition moment, to smoothly transition between three-dimensional and two-dimensional perspectives, maintaining pilot reference and situational awareness.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If abrupt transition between three-dimensional and two-dimensional perspectives is implemented, then switching speed between perspectives is improved, but pilot reference stability deteriorates causing harmful loss of reference

Engineering Contradiction:
Improveswitching speed between perspectivesVSAvoidpilot reference stability
Core Design Contradiction:
SpeedVSStability of the object's composition

Solution Approach 1:

The system dynamically adjusts the perspective transition by progressively modifying the opening angle and observation distance parameters. Instead of abrupt switching, the transition is made dynamic and continuous, allowing the display to adapt smoothly between 3D and 2D perspectives while maintaining pilot reference stability throughout the transition process.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The invention resolves the contradiction by changing key display parameters (opening angle and observation distance) during the transition. By progressively adjusting these parameters from their initial values to final values, the system enables smooth perspective transitions that maintain reference stability while achieving the desired switching between 3D and 2D views.

Inventive Principle:
Principle #35Parameter changes

2Stability of the object's composition

If three-dimensional synthesis images are displayed with fixed observation distance and opening angle, then image consistency is improved, but adaptability to different transition moments deteriorates

Engineering Contradiction:
Improveimage consistencyVSAvoidadaptability to different transition moments
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The system makes the observation distance and opening angle dynamic rather than fixed. These parameters are continuously adjusted as functions of the transition moment, allowing the image to adapt to different stages of the transition while maintaining overall consistency through controlled progression from initial to final parameter values.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The transition process is structured as a periodic sequence of parameter adjustments. The opening angle and observation distance are systematically modified at different transition moments, creating a structured progression that maintains image consistency while adapting to the specific requirements of each transition stage.

Inventive Principle:
Principle #19Periodic action

3Stability of the object's composition

If perspective transition is made smooth by progressive parameter adjustment, then pilot reference stability is improved, but transition time increases

Engineering Contradiction:
Improvepilot reference stabilityVSAvoidtransition time
Core Design Contradiction:
Stability of the object's compositionVSLoss of time

Solution Approach 1:

The system optimizes the balance between stability and time by strategically changing parameters (opening angle and observation distance) as functions of the transition moment. This allows the transition to be smooth and stable while controlling the overall transition time through efficient parameter progression.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS10861342B2System for displaying information related to a flight of an aircraft and associated method
Publication Date: 2020.12.08 DASSAULT AVIATION SA
  • US10861342B2 patent drawing
  • US10861342B2 patent drawing
  • US10861342B2 patent drawing

AI summary

A system for displaying information related to a flight of an aircraft and an associated method are provided. The display system comprises a dynamic synthesis image generating module, configured to generate at least two successive transition synthesis images between an image according to a first type of perspective and an image according to a second type of perspective, or between an image according to a second type of perspective and an image according to a first type of perspective, respectively, and to command the display thereof at successive transition moments. Each transition image is centered around an intermediate central point of interest, seen from an intermediate point of view situated at an intermediate observation distance from the intermediate central point of interest, which is an increasing function, a decreasing function, respectively, of the transition moment at which the image is displayed, and seen from an intermediate opening angle, which is a decreasing function, an increasing function, respectively, of the transition moment at which this image is displayed.