Auto-calibrating Drop Impact Sensor Using Accelerometer Bias Drift Cancellation

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Solution Overview

Problem

Current drop impact sensors for playground surfaces lack accuracy and precision due to the use of unsuitable accelerometer configurations, leading to potential underestimation of impact forces and increased risk of injuries, as they often require complex support mechanisms and introduce friction, which complicates testing and introduces errors.

Innovation Solution

A system utilizing a head form missile equipped with both high-g and low-g accelerometers, optimized with six accelerometers to improve measurement accuracy by canceling out bias drift and measuring deceleration forces more precisely, ensuring compliance with ASTM standards for impact attenuation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a three-axis accelerometer is used to detect impact forces, then the measurement can capture deceleration in all directions, but the device requires complex support mechanisms to maintain proper orientation during the drop test

Engineering Contradiction:
Improveimpact force measurement accuracyVSAvoidsupport mechanism complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent extracts the orientation maintenance function from a complex mechanical support mechanism and relocates it to a simple aerodynamic design feature - a fin attached to the accelerometer housing. This fin interacts with air resistance during the drop test to automatically align the accelerometer's Z-axis with the direction of motion, eliminating the need for complex mechanical guidance structures while maintaining measurement accuracy.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent replaces a mechanical support and guidance system with an aerodynamic solution. Instead of using mechanical guides or complex support structures to maintain accelerometer orientation, the invention uses air resistance acting on a fin to passively align the sensor axes with the motion direction, substituting mechanical complexity with a simpler fluid-dynamic approach.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Stability of the object's composition

If guide elements are used to maintain constant attitude during the drop, then the accelerometer orientation is stabilized, but friction is introduced which slows the impact tester and introduces measurement errors

Engineering Contradiction:
Improveaccelerometer orientation stabilityVSAvoidimpact measurement accuracy
Core Design Contradiction:
Stability of the object's compositionVSReliability

Solution Approach 1:

The patent converts the harmful effect of friction into a beneficial alignment mechanism. The fin, which would normally just create parasitic drag, is instead designed to interact with air resistance to automatically orient the accelerometer in the correct direction during the drop test. This transforms the aerodynamic drag from a harmful slowing force into a useful orientation-correcting force.

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

3Strength

If high-g accelerometers are used to measure impact forces, then the maximum acceleration can be detected, but the sensor becomes less sensitive to lower acceleration forces and introduces bias drift

Engineering Contradiction:
Improvemaximum acceleration detection capabilityVSAvoidlow acceleration measurement accuracy
Core Design Contradiction:
StrengthVSMeasurement precision

Solution Approach 1:

The patent segments the measurement function into two separate sensor systems: a high-g accelerometer for capturing maximum impact forces and a low-g accelerometer for measuring lower acceleration forces and providing calibration data. This segmentation allows each sensor to be optimized for its specific measurement range, with the low-g sensor compensating for the high-g sensor's bias drift and improving overall measurement accuracy across the full range of impact forces.

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 solution significantly enhances the accuracy and precision of drop impact sensing, providing reliable data on impact forces and reducing the risk of injuries by accurately measuring deceleration forces, thus ensuring playground surfaces meet safety standards.

Implementation Method 1

a three-axis accelerometer is attached near the center of gravity of the 'head form missile,' and the missile is dropped to the playground surface

Methodology Applied
Scientific EffectAccelerometer: Accelerometer

Implementation Method 2

the missile is dropped to the playground surface from the highest point on the play structure

Methodology Applied
Scientific EffectGravity: Gravitation

Data Source

PatentUS10746643B1Auto-calibrating drop impact sensor
Publication Date: 2020.08.18 BENTLEY ANTHONY EARL
  • US10746643B1 patent drawing
  • US10746643B1 patent drawing
  • US10746643B1 patent drawing

AI summary

A method and apparatus for improving the accuracy and precision of drop impact sensing data utilized for testing the impact-absorbing capacities of surfaces, especially playground surfaces used by children, for compliance with relevant standards. A head form missile is equipped with onboard sets of high-g and low-g accelerometers for timing a period of free-fall of the missile, as well as for measuring acceleration due to impact at the end of the fall. Optimized results are obtained in a preferred embodiment by exploiting at least four accelerometers. Three of the accelerometers are sized for “high-g” measurements in each axis (X-, Y-, and Z-axes). At least one “low-g” accelerometer for (measuring in the Z-axis), or three accelerometers sized for “low-g” measurements in all axis (X-, Y- and Z-axes) are employed. Accelerometer readings obtained during the “zero g” free-fall period is used to cancel bias drift on all accelerometers.