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JDWZZ1930B
Navigation / Mems / Imu

6-DoF MEMS IMU with ±400 or ±4000 °/s Gyroscope Range

MEMS Inertial Measurement Unit (IMU) · JDWZZ1930

Six-degree-of-freedom MEMS IMU combining a three-axis gyroscope (≤1 °/h zero bias stability) and three-axis accelerometer (≤100 µg zero bias stability) with 24-bit output and 1000 Hz sampling. Available in ±400 °/s and ±4000 °/s gyroscope range variants, with 10,000 g shock resistance for tactical navigation and stabilization.

Measurement Range

±400 °/s

Zero Bias Stability¹

≤1 °/h

Zero Bias Temperature Drift²

≤5 °/h

Product Gallery

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

Technical Specifications

Gyroscope Specifications

Measurement Range
±400 °/s
Zero Bias Stability¹
≤1 °/h
Zero Bias Temperature Drift²
≤5 °/h
Zero Bias g Sensitivity
≤1 °/h/g
Scale Factor Nonlinearity
≤100 ppm
Bandwidth
100 Hz
Resolution
24 bit

Accelerometer Specifications

Accelerometer Measurement Range
±20 g
Accelerometer Zero Bias Stability¹
≤100 μg
Zero Bias Temperature Coefficient
≤0.02 mg/°C
Scale Factor Nonlinearity
≤300 ppm
Bandwidth
100 Hz

Common Specifications

Sampling Rate³
1000 Hz
Activation Time
≤1 s
Power Supply Voltage
5~8 V
Current
≤300 mA
Operating Temperature
-40~+85 °C
Storage Temperature
-50~+90 °C
Resistant To Overload
≥10000 g

Gyroscope Specifications

Measurement Range
±4000 °/s
Zero Bias Stability¹
≤10 °/h
Zero Bias Temperature Drift²
≤50 °/h
Zero Bias g Sensitivity
≤10 °/h/g
Scale Factor Nonlinearity
≤150 ppm
Bandwidth
200 Hz
Resolution
24 bit

Accelerometer Specifications

Accelerometer Measurement Range
±20 g
Accelerometer Zero Bias Stability¹
≤100 μg
Zero Bias Temperature Coefficient
≤0.02 mg/°C
Scale Factor Nonlinearity
≤300 ppm
Bandwidth
100 Hz

Common Specifications

Sampling Rate³
1000 Hz
Activation Time
≤1 s
Power Supply Voltage
5~8 V
Current
≤300 mA
Operating Temperature
-40~+85 °C
Storage Temperature
-50~+90 °C
Resistant To Overload
≥10000 g
  1. [1]Zero bias stability figures use 10 s smoothing; temperature drift figures are 1σ over the full temperature range.
  2. [2]Sampling rate can be customized per project.

Technical Notes

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

Related Products

CGM300S10
MEMS / IMU

CGM300S10

Gyroscope Bias Stability (1σ)

0.05 °/hr

Angular Random Walk

0.02 °/√hr

Gyroscope Dynamic Range

±400 °/s

Accelerometer Bias Stability (1σ)

0.01 mg

CGM91AD10
MEMS / IMU

CGM91AD10

Measurement Range

±450 °/s

In-Run Bias Stability

≤1.0 °/h

Angular Random Walk

≤0.12 °/√h

Scale Factor Error

≤0.05 %

CGM92AD10
MEMS / IMU

CGM92AD10

Measurement Range

±450 °/s

In-Run Bias Stability

≤1.5 °/h

Angular Random Walk

≤0.15 °/√h

Scale Factor Error

≤0.1 %

Technical Documentation

Detailed documentation is shared directly with qualified B2B buyers after inquiry, under mutual confidentiality. Customer, supplier, and program information is never published.

Include the model number and your application in the inquiry form — an engineer will respond with the relevant documents.

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Datasheet (PDF)

Full performance curves, pinout diagrams, and environmental testing results.

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