Helmet Display Virtual Wingmen for Low Visibility Guidance

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Solution Overview

Problem

Low visibility conditions, such as harsh weather or dust, pose challenges for pilots in performing maneuvers like landing and navigating terrain at low altitudes, as existing visual guiding tools fail to provide effective conformal symbology for spatial reference.

Innovation Solution

A system that uses earth-space stabilized, 3D visual symbols resembling an aircraft, embedded within a pilot's helmet display, to provide dynamic reference points that update based on flight data and environmental conditions, ensuring conformity with the pilot's view and enhancing spatial perception.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional visual guiding tools are used in low visibility conditions, then pilots can see some reference indicators, but the indicators fail to provide effective conformal symbology for spatial reference

Engineering Contradiction:
Improvespatial reference accuracyVSAvoidguiding effectiveness in low visibility
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The patent creates virtual copies of aircraft (wingmen) that appear in the pilot's helmet display, copying the appearance and behavior of real aircraft to provide spatial reference. These virtual wingmen are rendered to match the pilot's perspective and aircraft formation geometry, creating realistic visual references that conform to the actual spatial relationships in the formation.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The system dynamically changes multiple parameters including the position, orientation, and visual properties of the symbology based on the pilot's line of sight, aircraft flight data, and formation geometry. The conformal nature of the display ensures that visual parameters remain accurate relative to the pilot's viewpoint and aircraft attitude throughout the maneuver.

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If conformal symbology is implemented to match pilot's view, then spatial reference accuracy improves, but the system complexity increases

Engineering Contradiction:
Improveconformal alignment accuracyVSAvoidhelmet display system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The helmet-mounted display acts as an intermediary between the formation geometry data and the pilot's visual perception. It processes aircraft position data, pilot heading, and formation parameters to generate the appropriate virtual wingmen symbology, translating complex spatial relationships into intuitive visual references that conform to the pilot's viewpoint.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent replaces physical visual aids (such as actual aircraft or traditional navigation equipment) with a digital rendering system that generates virtual wingmen through software. This substitution of mechanical/physical systems with computational rendering reduces the need for physical infrastructure while maintaining or improving spatial reference accuracy.

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

3Measurement precision

If dynamic updates based on flight data are implemented, then guiding accuracy in low visibility improves, but processing requirements and energy consumption increase

Engineering Contradiction:
Improvedynamic positioning accuracyVSAvoidhelmet display energy consumption
Core Design Contradiction:
Measurement precisionVSUse of energy by moving object

Solution Approach 1:

The system updates the virtual wingmen positions and orientations at regular intervals based on incoming flight data, rather than continuously rendering at maximum rate. This periodic updating maintains accurate spatial representation while reducing computational load and energy consumption compared to continuous high-frequency updates.

Inventive Principle:
Principle #19Periodic action

Data Source

PatentEP2543028B1System for guiding an aircraft to a reference point in low visibility conditions
Publication Date: 2019.06.26 ELBIT SYSTEMS LTD
  • EP2543028B1 patent drawingFigure 1~2
  • EP2543028B1 patent drawingFigure 3
  • EP2543028B1 patent drawingFigure 4

AI summary

A method of visually guiding a pilot flying an aircraft using one or more conformal symbols whose position is dynamically updated throughout the guidance is provided herein. The method includes the following stages: determining a desired flight route of an aircraft, based on a user-selected maneuver; presenting to a pilot, on a display, at least one 3D visual symbol that is: (i) earth-space stabilized, and (ii) positioned along a future location along the desired route; computing an updated desired route based on repeatedly updated aircraft flight data that include at least one of: location, speed, and spatial angle, of the aircraft; and repeating the presenting of the at least one 3D visual symbol with its updated location along the updated desired route.