Spinning Projectile Roll Estimation Under Magnetic Distortion

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Solution Overview

Problem

Accurate roll angle estimation in spinning projectiles is hindered by distortions in magnetic sensor data due to self-magnetic fields, sensor offsets, and induced magnetic fields, which affect the precision of steering commands.

Innovation Solution

A system and method that corrects magnetic sensor data by estimating and removing distortions such as permanent magnetic fields, induced magnetic fields, and sensor offsets, using known geomagnetic field vectors and angular velocity data to determine the roll angle and roll rate of the projectile, allowing for precise steering.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If magnetic sensor data is used to estimate roll angle, then steering commands can be generated, but distortion from self-magnetic fields reduces measurement precision

Engineering Contradiction:
Improveroll angle estimation accuracyVSAvoidself-magnetic field distortion
Core Design Contradiction:
Measurement precisionVSObject-generated harmful factors

Solution Approach 1:

The patent converts the harmful self-magnetic field distortion into a measurable quantity by using magnetic sensors to detect both the geomagnetic field and the projectile's self-magnetic field. By characterizing the distortion pattern during calibration and compensating for it during flight, the system transforms the harmful magnetic interference into useful information for improving roll angle estimation accuracy.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

2Measurement precision

If multiple distortion sources are corrected, then measurement precision improves, but device complexity increases

Engineering Contradiction:
Improvemagnetic sensor data accuracyVSAvoidcorrection process complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent merges multiple correction functions into a unified calibration and compensation process. During calibration, sensor offsets, permanent magnetic field distortions, and induced magnetic field coefficients are all estimated simultaneously through a series of maneuvers. During flight, these pre-calculated correction parameters are applied together to compensate for all distortion sources, reducing the operational complexity despite the multiple correction targets.

Inventive Principle:
Principle #5Merging (Combining)

3Measurement precision

If magnetic sensors are used in spinning projectiles, then roll angle can be estimated, but sensor offsets and induced magnetic fields cause errors

Engineering Contradiction:
Improveroll angle measurement accuracyVSAvoidsensor offset and induced magnetic field effects
Core Design Contradiction:
Measurement precisionVSObject-affected harmful factors

Solution Approach 1:

The patent performs preliminary calibration actions during controlled maneuvers (level flight, banked turns, inverted flight) to characterize and store correction parameters before actual flight operations. Sensor offsets, permanent magnetic field vectors, and induced magnetic field coefficients are all determined in advance through these calibration maneuvers, allowing the system to compensate for these harmful effects during normal flight without real-time complexity.

Inventive Principle:
Principle #10Preliminary action

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables accurate roll angle and roll rate estimation, ensuring that steering commands are applied in the proper direction, thereby improving the trajectory control of spinning projectiles.

Implementation Method 1

estimating, with the at least magnetic sensor, a magnetic data output associated with a local magnetic field relative to the spinning projectile

Methodology Applied
Scientific EffectMagnetic field detection: Magnetic Field

Implementation Method 2

the first source of distortion is a permanent magnetic field of the spinning projectile

Methodology Applied
Scientific EffectPermanent magnetic field: Magnetism

Implementation Method 3

magnetic fields produced by eddy currents on the spinning shell body

Methodology Applied
Scientific EffectEddy currents: Eddy Currents

Implementation Method 4

estimating, with at least one angular rate sensor, a roll rate of the spinning projectile

Methodology Applied
Scientific EffectAngular velocity detection: Gyroscope

Data Source

PatentUS10907936B2State estimation
Publication Date: 2021.02.02 BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC
  • US10907936B2 patent drawing
  • US10907936B2 patent drawing
  • US10907936B2 patent drawing

AI summary

A system and method for state estimation in spinning projectiles is provided. The state estimation is based, at least in part, on magnetic sensor data, angular velocity data, and correction terms applied to the magnetic sensor data and the angular velocity data. The system and method for state estimation in spinning projectiles estimates roll angles and roll rates of the spinning projectiles. The roll angle and roll rate estimates allow steering commands to be applied to steer the spinning projectiles in the proper direction.