Magnetic Anomaly Map Conversion for Stable Altitude Navigation

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Solution Overview

Problem

Existing methods for lifting and lowering magnetic anomalies in magnetic navigation systems, such as the Fast-Fourier-Transform (FFT) method, are inaccurate and unstable, introducing constant biases and errors, particularly when converting between latitude-longitude-altitude (LLA) and Earth-Centered Earth-Fixed (ECEF) coordinates.

Innovation Solution

The use of the Strakhov integration method in conjunction with Earth-Centered Earth-Fixed (ECEF) coordinates to accurately lift and lower magnetic anomalies, employing a two-step process to convert 2D maps from LLA to ECEF coordinates and perform Strakhov iterations to compute magnetic anomalies, allowing for accurate navigation at various altitudes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If the FFT method is applied to lift magnetic anomalies from anomaly maps, then computational efficiency is improved, but measurement precision deteriorates due to introduction of constant bias and errors

Engineering Contradiction:
Improvecomputational efficiencyVSAvoidmagnetic anomaly accuracy
Core Design Contradiction:
ProductivityVSMeasurement precision

Solution Approach 1:

The patent introduces an intermediary coordinate transformation step that converts magnetic anomaly data from LLA coordinates to a local tangent plane coordinate system before applying FFT. This intermediary transformation resolves the coordinate system incompatibility that causes FFT to introduce bias, thereby maintaining both computational efficiency and measurement precision.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent changes the coordinate system parameters from global LLA coordinates to local tangent plane coordinates, and adjusts the FFT application parameters to match the transformed coordinate system. This parameter change eliminates the fundamental incompatibility between FFT assumptions and LLA coordinate geometry, resolving the precision issue while preserving computational efficiency.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If the FFT method is used to lower magnetic anomalies to altitudes below the reference map altitude, then computational speed is maintained, but reliability deteriorates due to instability

Engineering Contradiction:
Improvecomputational speedVSAvoidmagnetic anomaly computation stability
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The patent applies preliminary coordinate transformation and bias correction operations before the FFT lowering process to counteract the instability that would otherwise occur. By preparing the data in advance with appropriate transformations, the method prevents the reliability issues that arise during the lowering operation while maintaining computational speed.

Inventive Principle:
Principle #9Preliminary anti-action

3Ease of operation

If magnetic anomaly maps in LLA coordinates are processed directly by FFT, then ease of operation is maintained, but manufacturing precision deteriorates due to coordinate system incompatibility

Engineering Contradiction:
Improvedirect FFT applicationVSAvoidmagnetic anomaly map accuracy
Core Design Contradiction:
Ease of operationVSManufacturing precision

Solution Approach 1:

The patent performs preliminary coordinate transformation from LLA to tangent plane coordinates, and pre-computes correction factors, before applying FFT to the magnetic anomaly data. This preliminary preparation maintains ease of operation by automating the transformation process while ensuring manufacturing precision through proper coordinate system alignment.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS12560433B2Methods for lifting and lowering magnetic anomalies for magnetic navigation
Publication Date: 2026.02.24 HONEYWELL INTERNATIONAL INC
  • US12560433B2 patent drawing
  • US12560433B2 patent drawing
  • US12560433B2 patent drawing

AI summary

A system and method for magnetic navigation are provided. The system comprises a navigation system for a vehicle, at least one processor operatively coupled with the navigation system, and a magnetic navigation module operatively coupled with the processor. The magnetic navigation module including instructions, executable by the processor, to perform a method comprising selecting latitude, longitude, and altitude ranges for the vehicle that is expected to travel in a region of interest; obtaining one or more magnetic anomaly maps for the region of interest; choosing a base Earth-centered, Earth-fixed (ECEF) plane and coordinates for the one or more magnetic anomaly maps; constructing an integration mesh on the base ECEF plane; and performing a Strakhov iteration process on the integration mesh to compute values of magnetic anomalies on a base source. The method then computes an estimated magnetic anomaly at a given point in space using alternative computation approaches.