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D-Q-JDW-ZZ1930

JDWZZ1930B

Advanced 6-DOF MEMS IMU integrating three-axis gyroscope and accelerometer, featuring superior zero bias stability, excellent scale factor characteristics, and outstanding shock resistance capable of withstanding environments exceeding 10000g

JDWZZ1930B

Customizable Parameters

Specifications shown are reference configurations. Most parameters can be adjusted to meet your application requirements.

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The JDWZZ1930A is a high-precision six-degree-of-freedom inertial measurement unit designed for accurate motion sensing and orientation determination. This advanced system integrates a three-axis MEMS gyroscope with ±400°/s measurement range and exceptional zero bias stability (≤1°/h), alongside a three-axis MEMS accelerometer with ±20g measurement range and superior stability (≤100μg). The comprehensive integration of sensing elements with sophisticated signal processing circuitry delivers outstanding performance for demanding applications requiring precise motion tracking and inertial navigation capabilities.

Key Features

  • Three-axis MEMS gyroscope with ±400°/s measurement range
  • Exceptional zero bias stability (≤1°/h)
  • Minimal temperature drift (≤5°/h across full temperature range)
  • Low g-sensitivity (≤1°/h/g)
  • Excellent scale factor linearity (≤100ppm nonlinearity)
  • Three-axis MEMS accelerometer with ±20g measurement range
  • Superior zero bias stability (≤100μg)
  • Low temperature coefficient (≤0.02mg/°C)
  • Excellent scale factor linearity (≤300ppm nonlinearity)
  • Complete six-degree-of-freedom measurement capability
  • High-resolution 24-bit data output
  • Fast 1000Hz sampling rate
  • Advanced signal processing and filtering
  • Wide operating temperature range (-40~+85°C)
  • Exceptional shock resistance (≥10000g)

Applications

Tactical-grade inertial navigation systemsHigh-precision attitude determinationIndustrial robotics requiring accurate positioningStabilization systems for precision equipmentVehicle dynamics testing with high accuracy requirementsUAV and drone navigation in high-maneuverability scenariosSports and high-motion analysis systemsRacing and high-dynamic vehicle testingStabilization systems for fast-moving platformsVibration monitoring in industrial machineryIndustrial automation and control systemsPrecision agriculture equipmentLand vehicle navigation supplementsAntenna and platform stabilizationShort-term navigation during GNSS outages

Specifications

Gyroscope Specifications

Measurement Range°/s±400
Zero Bias Stability¹°/h≤1
Zero Bias Temperature Drift²°/h(1σ)≤5
Zero Bias g Sensitivity°/h/g≤1
Scale Factor Nonlinearityppm≤100
BandwidthHz100
Resolutionbit24

Accelerometer Specifications

Measurement Rangeg±20
Zero Bias Stability¹μg≤100
Zero Bias Temperature Coefficientmg/°C≤0.02
Scale Factor Nonlinearityppm≤300
BandwidthHz100

Common Specifications

Sampling Rate³Hz1000
Activation Times≤1
Power Supply VoltageV5~8
CurrentmA≤300
Operating Temperature°C-40~+85
Storage Temperature°C-50~+90
Resistant To Overloadg≥10000

Gyroscope Specifications

Measurement Range°/s±4000
Zero Bias Stability¹°/h≤10
Zero Bias Temperature Drift²°/h(1σ)≤50
Zero Bias g Sensitivity°/h/g≤10
Scale Factor Nonlinearityppm≤150
BandwidthHz200
Resolutionbit24

Accelerometer Specifications

Measurement Rangeg±20
Zero Bias Stability¹μg≤100
Zero Bias Temperature Coefficientmg/°C≤0.02
Scale Factor Nonlinearityppm≤300
BandwidthHz100

Common Specifications

Sampling Rate³Hz1000
Activation Times≤1
Power Supply VoltageV5~8
CurrentmA≤300
Operating Temperature°C-40~+85
Storage Temperature°C-50~+90
Resistant To Overloadg≥10000

Technical Notes

  1. 10s smoothing 2. Full temperature 3. Sampling rate can be customized

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All specifications can be customized. Tell us your requirements for a tailored solution.