Editorial Technical Reference

Triaxial Gyroscope

This page explains how Triaxial Gyroscope is classified within Computer, Electronic and Optical Product Manufacturing. Technical values and manufacturer relationships are research references; confirm the current specification and supplier evidence for each order.

Technical Definition & Core Assembly

The triaxial gyroscope is a component used in the manufacturing of computer, electronic, and optical products.

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Product Specifications

Technical details and manufacturing context for Triaxial Gyroscope

Definition
The triaxial gyroscope is a component used in the manufacturing of computer, electronic, and optical products. It is a core part of an Inertial Measurement Unit (IMU) that detects and measures the rate of rotation or angular velocity in three-dimensional space. By sensing changes in angular momentum, it provides critical orientation and rotational motion data. The device typically uses MEMS (Micro-Electro-Mechanical Systems) or optical principles, such as fiber optic gyroscopes (FOG). The gyroscope operates by detecting the Coriolis effect on a vibrating or rotating proof mass. When the device rotates, the Coriolis force induces a secondary vibration perpendicular to the drive direction, which is measured to determine angular velocity. Modern triaxial gyroscopes often integrate three single-axis sensing elements onto a single MEMS chip. The product is available with selectable full-scale measurement ranges from ±250 to ±2000 degrees per second. Bias stability, measured by Allan variance at constant temperature, is ≤0.8 degrees per hour. Angular random walk noise density is ≤0.2 degrees per square root hour. Nonlinearity, based on best fit straight line, is ≤0.1% of full scale. The bandwidth is configurable via a low-pass filter from 100 to 500 Hz. Supply voltage ranges from 3.0 to 5.5 V DC, with current consumption ≤10 mA at 3.3 V. Operating temperature range is -40 to 85 °C. The device can survive shocks of 10000 g (0.1 ms half-sine). Digital output interfaces include SPI and I2C. Package size is LCC-16, measuring 4.5×4.5×1.0 mm, and weight is ≤0.5 g without PCB. Materials used include silicon (MEMS), piezoelectric materials, and optical fibers (for FOG). These specifications are directory reference ranges; verify model-specific values with the legal manufacturer or supplier before procurement.
Working Principle
The triaxial gyroscope operates by detecting the Coriolis effect on a vibrating or rotating proof mass. When the device rotates, the Coriolis force causes a secondary vibration perpendicular to the drive direction, which is measured to determine angular velocity. Modern triaxial gyroscopes often integrate three single-axis sensing elements onto a single MEMS chip.
Common Materials
Silicon (MEMS), Piezoelectric materials, Optical fibers (for FOG)
Technical Parameters
ParameterTypical rangeNotes & selection driver
Measurement Range±250–±2000 °/sSelectable full-scale range
Bias Stability≤0.8 °/hAllan variance at constant temperature
Angular Random Walk≤0.2 °/√hNoise density
Nonlinearity≤0.1 % FSBest fit straight line
Bandwidth100–500 HzConfigurable low-pass filter
Supply Voltage3.0–5.5 V DCInternal regulator
Current Consumption≤10 mAAt 3.3 V
Operating Temperature-40–85 °CFull performance
Shock Survivability10000 g0.1 ms half-sine
InterfaceSPI/I2CDigital output
Package Size4.5×4.5×1.0 mmLCC-16
Weight≤0.5 gWithout PCB

Ranges are indicative industry figures for RFQ preparation, not a supplier commitment. Confirm every value and standard with the legal manufacturer before ordering.

Components / BOM
  • Proof Mass Part
    Vibrating element that experiences Coriolis force during rotation
    Material: Silicon
  • Drive Electrodes Part
    Electrostatically drive the proof mass into resonance
    Material: Doped silicon with metal contacts
  • Sense Electrodes Part
    Detect displacement of proof mass caused by Coriolis force
    Material: Doped silicon with metal contacts
  • ASIC
    Application-Specific Integrated Circuit for signal conditioning and digitization
    Material: Semiconductor (silicon)
  • Package Part
    Protects the MEMS die and provides electrical connections
    Material: Ceramic or plastic

Industry Taxonomies & Aliases

Commonly used trade names and technical identifiers for Triaxial Gyroscope.

Applied To / Applications

This component is essential for the following industrial systems and equipment:

Industrial Ecosystem & Supply Chain Structure

Complementary Systems
Downstream Applications
Specialized Tooling

Application Fit & Sizing Matrix

Operational Limits
pressure: Atmospheric to 1.5 bar absolute (typical), up to 3 bar for specialized models
other spec: Angular velocity range: ±300°/s to ±2000°/s (selectable), bandwidth: 10-100 Hz, vibration tolerance: 20g RMS
temperature: -40°C to +85°C (operational), -55°C to +125°C (storage)
Media Compatibility
✓ Aerospace navigation systems ✓ Industrial robotics ✓ Automotive stability control systems
Unsuitable: High-pressure hydraulic fluid environments with rapid pressure fluctuations
Sizing Data Required
  • Required angular velocity measurement range (±°/s)
  • Desired bandwidth/frequency response (Hz)
  • Environmental vibration levels (g RMS)

Reliability & Engineering Risk Analysis

Failure Mode & Root Cause
Gyroscopic Drift
Cause: Mechanical wear in bearings or gimbals causing friction, thermal expansion mismatches in MEMS structures, or electronic component aging leading to calibration errors.
Sensor Signal Degradation
Cause: Contamination ingress (dust, moisture) affecting MEMS elements, vibration-induced fatigue in microstructures, or electrical interference from nearby equipment disrupting signal integrity.
Maintenance Indicators
  • Unstable or erratic output readings during stationary operation
  • Audible grinding or clicking noises from the housing during rotation
Engineering Tips
  • Implement regular calibration cycles using precision test equipment and maintain strict environmental controls (temperature, humidity, vibration isolation) to minimize drift sources.
  • Use conformal coating on electronic components, install proper EMI shielding, and follow manufacturer-specified mounting procedures to prevent mechanical stress and contamination.

Indicative industry ranges for design and RFQ preparation. Confirm the exact figures and applicable standard with the manufacturer before specifying.

Compliance & Manufacturing Standards

Applicable Standards
ISO 8727:1997 - Mechanical vibration and shock - Balancing of rotating rigid bodies ANSI/ISA-37.1-1975 (R2018) - Specifications and Tests for Piezoelectric Acceleration Transducers DIN EN 60068-2-6:2008 - Environmental testing - Part 2-6: Tests - Test Fc: Vibration (sinusoidal)

Quoted from the published standard.

Manufacturing Precision
  • Angular Rate Bias Stability: +/- 0.1°/s
  • Alignment Error: +/- 0.05°
Quality Inspection
  • Temperature Cycling Test (-40°C to +85°C)
  • Vibration Test (20-2000 Hz, 10 g RMS)

Manufacturers of Triaxial Gyroscope

Manufacturer profiles associated with Triaxial Gyroscope.

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Frequently Asked Questions

What is the measurement range of this triaxial gyroscope?

The selectable full-scale measurement range is ±250 to ±2000 degrees per second. This is a directory reference; confirm the exact range for the specific model with the manufacturer.

What interfaces does the gyroscope support?

The digital output interfaces are SPI and I2C. These are standard serial interfaces for connecting to microcontrollers or processors.

What is the operating temperature range?

The operating temperature range is -40 to 85 °C for full performance. Ensure the application environment stays within this range.

How should I verify the bias stability specification?

Bias stability is specified as ≤0.8 °/h, measured using Allan variance at constant temperature. For your application, request the manufacturer's test data and verification method.

Data Basis

Editorial classification, named public sources where available, and source-reviewed manufacturer records.

Preliminary Technical Classification
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