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Asset ID: mems-imu-micro-zz3415
JDWZZ3415
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JDWZZ3415

Advanced MEMS micro-IMU integrating three-axis gyroscope (±3600°/s) and three-axis accelerometer (±20g), featuring superior stability and precision performance

Measurement Range

+3600 -3600

Scale Factor

2010 1990

Scale Factor Nonlinearity

150

The JDWZZ3415 is a high-performance MEMS micro-inertial measurement unit integrating three-axis gyroscope and three-axis accelerometer capabilities. The gyroscope system provides ±3600°/s measurement range with excellent scale factor characteristics (nonlinearity ≤150ppm) and superior zero bias stability (≤10°/h with 10s smoothing). The accelerometer system offers ±20g measurement range with high precision (scale factor nonlinearity ≤150ppm) and exceptional stability (zero bias stability ≤0.1mg). Housed in a lightweight super-hard aluminum case with potting protection, the unit features integrated control and signal processing circuits for comprehensive inertial measurement capabilities.

Key Features

  • Integrated three-axis gyroscope and accelerometer systems
  • High-performance gyroscope specifications:
  • Wide measurement range: ±3600°/s
  • Superior scale factor accuracy (1990-2010 LSB/°/s)
  • Excellent scale factor nonlinearity (≤150ppm)
  • Outstanding zero bias stability (≤10°/h)
  • High bandwidth (180-220Hz)
  • High-precision accelerometer specifications:
  • Wide measurement range: ±20g
  • Precise scale factor (39900-40100 LSB/g)
  • Superior scale factor nonlinearity (≤150ppm)
  • Excellent zero bias stability (≤0.1mg)
  • High bandwidth (80-120Hz)
  • Advanced mechanical design:
  • Lightweight super-hard aluminum construction
  • Internal potting protection
  • High overload resistance (≥20000g)
  • Comprehensive performance features:
  • Wide operating temperature range (-40°C to +60°C)
  • Fast activation time (≤1s)
  • Stable power supply requirements (4.85-5.05V)

Applications

Inertial navigation systemsAttitude and heading reference systemsMulti-axis motion tracking and controlHigh-precision platform stabilizationAdvanced robotics navigationUnmanned vehicle control systemsAerospace motion sensingHigh-dynamic testing and measurement

Technical Specifications

Gyroscope Specifications

Measurement Range

+3600

-3600

Scale Factor

2010

1990

Scale Factor Nonlinearity

150

Zero Bias¹

0.05

-0.05

Zero Bias Stability (10s Smoothing)

10

Zero Bias Temperature Coefficient²

1

Zero Bias g Sensitivity

10

Bandwidth

220

180

Accelerometer Specifications

Measurement Range

20

-20

Scale Factor

40100

39900

Scale Factor Nonlinearity

150

Zero Bias¹

5

-5

Zero Bias Stability (10s Smoothing)

0.1

Bandwidth

120

80

Orthogonality

6

Common Specifications

Power Supply Voltage

5.05

4.85

Operating Temperature

+60

-40

Activation Time

1

Resistant To Overload

-

20000

Technical Notes

  1. Full temperature, 2℃/min temperature change rate 2. Measurement temperature points are: -40℃,25℃,60℃

Technical Documentation

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Datasheet (PDF)

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

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CAD Model (STEP)

High-fidelity 3D geometry for structural integration and thermal modeling.

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Compliance Documentation

Certification of origin, quality management protocols, and compliance documentation.

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