Projectile Sensor Fusion Layout for Spin Noise and Drift

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Solution Overview

Problem

Existing guidance systems for munitions face issues with high-frequency noise in accelerometers and drift in gyroscopes, which degrade accuracy during various flight maneuvers, particularly high spin rates and aggressive maneuvers.

Innovation Solution

A sensor farm comprising gyroscopes, accelerometers, and magnetometers with overlapping ranges and individual calibration, using sensor averaging and fusion techniques to combine data, mitigating noise and bias drift, and employing lead solder connections for shock resistance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If accelerometers are used to measure high spin rates, then angular velocity measurement capability is improved, but high-frequency noise increases

Engineering Contradiction:
Improveangular velocity measurement capabilityVSAvoidhigh-frequency noise
Core Design Contradiction:
SpeedVSObject-generated harmful factors

Solution Approach 1:

The patent combines multiple accelerometer types (analog and digital) with different measurement ranges and characteristics into a unified sensor farm. By merging sensors with complementary strengths, the system can select appropriate sensors based on flight conditions, using low-range sensors for low-speed phases and high-range sensors for high-speed phases, thereby reducing noise while maintaining measurement capability across the full speed range.

Inventive Principle:
Principle #5Merging (Combining)

2Measurement precision

If gyroscopes are used to measure angular acceleration, then orientation measurement capability is improved, but bias drift increases

Engineering Contradiction:
Improveorientation measurement capabilityVSAvoidbias drift
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The patent introduces magnetometers as intermediary sensors to compensate for gyroscope drift. The magnetometer provides absolute orientation reference by measuring the Earth's magnetic field, serving as a mediator that corrects the accumulated errors in gyroscope measurements. This combination allows the system to maintain high orientation measurement precision while eliminating the bias drift problem through periodic recalibration using the magnetic field reference.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Measurement precision

If multiple sensors with overlapping ranges are used, then measurement accuracy is improved, but device complexity increases

Engineering Contradiction:
Improvemeasurement accuracyVSAvoidsensor farm complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent implements dynamic sensor selection and fusion where the system adaptively chooses which sensors to use based on real-time flight conditions. During low-speed phases, low-range sensors are activated; during high-speed phases, high-range sensors are activated. This dynamic approach allows the system to maintain high measurement accuracy across all flight regimes while managing complexity by not all sensors operating simultaneously at full capacity.

Inventive Principle:
Principle #15Dynamics

4Measurement precision

If sensors are positioned offset from center of spin, then centripetal spin measurement is improved, but susceptibility to shock increases

Engineering Contradiction:
Improvecentripetal spin measurementVSAvoidshock susceptibility
Core Design Contradiction:
Measurement precisionVSObject-affected harmful factors

Solution Approach 1:

The patent segments the sensor farm into multiple groups positioned at different locations relative to the center of spin. Some sensors are placed offset to capture centripetal acceleration components, while others are positioned closer to the center to minimize shock exposure. This segmentation allows the system to obtain accurate centripetal spin measurements from offset sensors while using centrally-positioned sensors as backup during high-shock phases, thereby resolving the contradiction between measurement precision and shock susceptibility.

Inventive Principle:
Principle #1Segmentation

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

The system provides a more accurate and reliable measurement of projectile position, velocity, and orientation by compensating for sensor weaknesses, enhancing precision and reliability under extreme conditions.

Implementation Method 1

high angular velocity measurements are improved by offsetting the plurality of accelerometers from a center of spin to obtain centripetal spin

Methodology Applied
Scientific EffectCentripetal acceleration: Centrifugal Force

Implementation Method 2

a second type being a gyroscope, the gyroscope providing angular acceleration data

Methodology Applied
Scientific EffectGyroscope effect: Gyroscope

Implementation Method 3

a third type being a magnetometer, the magnetometer providing position data relative to a fixed magnetic field

Methodology Applied
Scientific EffectMagnetic field sensing: Magnetic Field

Implementation Method 4

the sensors are fixed to the circuit with lead solder with sufficient malleability to withstand a high shock environment

Methodology Applied
Scientific EffectMalleability: Plasticity

Data Source

PatentUS12487056B2Sensor farm
Publication Date: 2025.12.02 USA AS REPRESENTED BY THE SECRETARY OF THE NAVY
  • US12487056B2 patent drawing
  • US12487056B2 patent drawing
  • US12487056B2 patent drawing

AI summary

An apparatus that includes at least two types of sensors arranged on a projectile, each type of sensor including a plurality of sensors with overlapping ranges.