Avionics Display Geodetic Datum Compliance Detection

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Solution Overview

Problem

Current aircraft navigation systems lack a mechanism to differentiate between compliant and non-compliant regions for Global Navigation Satellite System (GNSS) navigation, leading to potential inaccuracies during landing approaches, especially in areas using non-standard geodetic reference systems like Russia and China.

Innovation Solution

A system comprising a route compliance module that defines a geodetic reference datum standard, a navigation system database with compliance information, and a flight management system to identify and visually differentiate non-compliant regions on a coverage map, adjusting the display to indicate non-compliant areas and disabling GPS approaches when necessary.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If GPS based navigation is used in countries using non-WGS-84 geodetic reference systems, then navigation coverage is maintained, but position accuracy deteriorates due to datum incompatibility

Engineering Contradiction:
Improvenavigation coverage areaVSAvoidposition accuracy
Core Design Contradiction:
Area of stationary objectVSMeasurement precision

Solution Approach 1:

The system applies different geodetic reference datums to different geographical regions. The FMS stores multiple datum information (WGS-84 and local datums like PZ-90) and automatically selects the appropriate datum based on the current flight location and airport of destination, ensuring position accuracy is maintained locally in each region while preserving global navigation coverage

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The system changes the geodetic reference datum parameter based on location. The route compliance module queries the navigation database to determine which datum applies to the current region and adjusts the coordinate system accordingly, transforming position data between different datums to maintain measurement precision across different geographical areas

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If pilots manually deselect GPS before approach in non-compliant areas, then position accuracy is improved, but navigation efficiency deteriorates due to additional manual intervention

Engineering Contradiction:
Improveposition accuracyVSAvoidnavigation efficiency
Core Design Contradiction:
Measurement precisionVSProductivity

Solution Approach 1:

The FMS automatically performs datum selection and coordinate transformation without pilot intervention. The route compliance module autonomously queries the navigation database, determines the appropriate datum for the current region and destination airport, and adjusts the navigation system accordingly, eliminating the need for manual GPS deselection while maintaining position accuracy

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system provides feedback to the pilot about the geodetic reference datum status. The display system shows information about WGS-84 compliance status and automatically adjusts navigation parameters based on the determined datum, giving the pilot awareness of the system's automatic actions while maintaining navigation efficiency

Inventive Principle:
Principle #23Feedback

3Measurement precision

If compliance information is stored in the navigation database, then position accuracy is improved, but system complexity increases due to additional data management requirements

Engineering Contradiction:
Improveposition accuracyVSAvoiddata management complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system merges geodetic reference datum compliance information with the existing navigation database structure. The route compliance module integrates datum information alongside existing navigation data (waypoints, airports, routes), utilizing the same database query mechanisms and storage structures already present in the FMS, thereby avoiding additional complex data management systems while improving position accuracy

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS10176721B2System and method to depict geodetic reference datum non-compliance regions, airports, and flight planning elements on avionics based displays
Publication Date: 2019.01.08 HONEYWELL INTERNATIONAL INC
  • US10176721B2 patent drawing
  • US10176721B2 patent drawing
  • US10176721B2 patent drawing

AI summary

Systems and methods are provided for displaying portions of a route on a coverage map that are non-compliant for a Global Navigation Satellite System (GNSS) navigation system in an aircraft. A route compliance module defines a geodetic reference datum standard based on the GNSS navigation system. A navigation system database has compliance information corresponding to each of a plurality of airports. A flight management system determines the route of the aircraft and a visual display displays the route and the coverage map. The route compliance module identifies a non-compliant region of the coverage map that is not compliant with the geodetic reference datum standard based on the compliance information and adjusts the visual display to differentiate a non-compliant portion of the route extending within the non-compliant region of the coverage map.