Avionics Display System for Predictive Landing Site Cues

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Solution Overview

Problem

Modern avionics display systems lack predictive visual guidance for pilots executing a safe landing after an engine failure, as they do not effectively display potential landing sites resulting from various aircraft configurations in a conformal, three-dimensional graphical format.

Innovation Solution

An avionics display system that processes avionics data to determine the current aircraft configuration, predict landing sites based on different configurations, and display predictive cues on a three-dimensional graphical terrain display, including symbols and text indicating potential landing locations associated with various lift-to-drag ratio alterations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If modern avionics display systems display considerable amount of useful information, then information availability is improved, but predictive visual guidance for landing sites is still lacking

Engineering Contradiction:
Improveinformation availabilityVSAvoidpredictive visual guidance
Core Design Contradiction:
Quantity of substanceVSLoss of information

Solution Approach 1:

The system performs preliminary calculations to predict multiple potential landing sites based on current aircraft configuration and various configuration changes. These predicted landing sites are displayed in advance to the pilot, allowing proactive decision-making about configuration changes before they are actually made, rather than reacting after the fact.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system adds a new dimension of predictive information to the traditional avionics display by showing not just current position and terrain, but also predicted landing sites for different configurations. This transforms the display from a static representation to a dynamic predictive tool that shows multiple possible outcomes.

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

2Ease of operation

If pilots make various aircraft configuration changes during glide landing, then landing control is improved, but landing location predictability worsens

Engineering Contradiction:
Improvelanding controlVSAvoidlanding location predictability
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The system provides feedback to the pilot by displaying predicted landing sites for different configuration options. This allows the pilot to see the consequence of each potential configuration change on the landing location, enabling informed decision-making about which configuration to select based on the desired landing area.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system calculates and displays multiple predicted landing sites in advance for different configuration scenarios, allowing the pilot to plan configuration changes proactively rather than reactively, improving both control and predictability.

Inventive Principle:
Principle #10Preliminary action

3Productivity

If aircraft configuration changes are made during glide, then glide performance is optimized, but landing site location changes

Engineering Contradiction:
Improveglide performanceVSAvoidlanding site location
Core Design Contradiction:
ProductivityVSMeasurement precision

Solution Approach 1:

The system adds the dimension of predictive landing site visualization to show how different configuration choices affect landing location. This allows pilots to optimize glide performance while simultaneously understanding the impact on landing site, making informed trade-offs.

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

Solution Approach 2:

The system provides immediate visual feedback showing the relationship between configuration changes and resulting landing site locations, enabling pilots to make real-time decisions that balance glide performance optimization with landing site selection.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS9418561B2System and method for displaying predictive conformal configuration cues for executing a landing
Publication Date: 2016.08.16 HONEYWELL INTERNATIONAL INC
  • US9418561B2 patent drawing
  • US9418561B2 patent drawing
  • US9418561B2 patent drawing

AI summary

A system and method for displaying predictive cues on an aircraft display system for executing a landing after an engine failure is provided. The system and method displays the cues for various aircraft configurations, and each cue is displayed in perspective (conformally) on a three dimensional graphical display of the surrounding terrain.