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JDWZZ3415
Navigation / Mems / Imu

Micro 6-DoF MEMS IMU (±3600 °/s, ±20 g)

MEMS Inertial Measurement Unit (IMU) · JDWZZ3415

Micro six-degree-of-freedom MEMS IMU in a lightweight potted aluminum package, with ±3600 °/s gyroscope range (≤10 °/h zero bias stability, 10 s smoothing) and ±20 g accelerometer range (≤0.1 mg zero bias stability). Fast ≤1 s activation and 20,000 g overload resistance for high-dynamic navigation and stabilization.

Measurement Range

±3600 °/s

Scale Factor

1990–2010 LSB/(°/s)

Scale Factor Nonlinearity

≤150 ppm

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 °/s
Scale Factor
1990–2010 LSB/(°/s)
Scale Factor Nonlinearity
≤150 ppm
Zero Bias¹
±0.05 °/h
Zero Bias Stability (10s Smoothing)
≤10 °/h
Zero Bias Temperature Coefficient²
≤1 °/h/°C
Zero Bias g Sensitivity
≤10 °/h/g
Bandwidth
180–220 Hz

Accelerometer Specifications

Accelerometer Measurement Range
±20 g
Scale Factor
39900–40100 LSB/g
Scale Factor Nonlinearity
≤150 ppm
Zero Bias¹
±5 mg
Accelerometer Zero Bias Stability (10s Smoothing)
≤0.1 mg
Bandwidth
80–120 Hz
Orthogonality
6 °

Common Specifications

Power Supply Voltage
4.85–5.05 V
Operating Temperature
-40~+60 °C
Activation Time
≤1 s
Resistant To Overload
≥20000 g
  1. [1]Zero bias stability is specified with 10 s smoothing; full-temperature figures apply at a 2 °C/min temperature change rate.
  2. [2]Bandwidth is configuration-dependent (180–220 Hz gyroscope, 80–120 Hz accelerometer).

Technical Notes

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

Related Products

CGM300S10
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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
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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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