Spirit10E-RL
Spirit10E-RL_Datasheet_Product Manual-V1.1
File size： 1.9MB
Upload time：Mar 26,2026
Product Overview
The Spirit10E-RL is a complete inertial measurement unit that includes a three-axis gyroscope and a three-axis accelerometer. Each inertial sensor in the Spirit10E-RL integrates industry-leading MEMS technology with signal-processing algorithms optimized for superior dynamic performance. Factory calibration corrects for each sensor’s sensitivity, bias, and inter-axis coupling, ensuring that every sensor delivers highly accurate measurements.
The Spirit10E-RL offers a simple and cost-effective solution for integrating precise multi-axis inertial sensing into industrial systems, with particular advantages in applications that require attitude output. All necessary motion testing and calibration are performed as part of the factory production process, significantly reducing system integration time and freeing up processing resources on the host control chip. Tight orthogonal alignment simplifies the alignment of the inertial frame within navigation systems. UART and CAN interfaces provide straightforward interfaces for data acquisition and configuration control. The Spirit10E-RL module measures approximately 30 mm × 30 mm × 10.6 mm and is equipped with standard interfaces.
Product Features
- Three-axis digital gyroscope, range ±4000 deg/s
- <0.05° inter-axis coupling error
- 1.4 deg/h bias instability
- 0.15 deg/h angular random walk
- <100 ppm scale factor nonlinearity
- Three-axis digital accelerometer, range ±16g
- Factory-calibrated sensitivity, zero offset, and inter-axis coupling correction
- Calibration temperature range: -40°C to +85°C
- UART and CAN protocol support
- Configurable high- and low-pass digital filters
- Alarm for Condition Monitoring
- High-frequency attitude output up to 1000 Hz
- Data-ready functionality
- Single-command self-test
- Single-supply operation: 4.0 V to 6.0 V
- 2000g Vibration Resistance
- Operating temperature range: -40°C to +85°C
Product Applications
- Agriculture and Mechanical Engineering
- High-precision navigation
- Platform Stability and Control
- Robot
- Autonomous vehicle
- Motion and Position Monitoring
- Inclination measurement
Product Information
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- Accelerometer parameters
- Spinning Top Parameters
Parameters Test Conditions Minimum value Typical value Maximum value Unit Acceleration range ±2 g ±4 g ±8 g ±16 g Scale factor error 0.1 0.15 % Zero-bias repeatability National Military Standard 0.18 0.2 milligram Full-temperature zero-bias error -40~85℃ 10s
Smooth, 1 σ1.5 2 milligram Scale factor nonlinearity 0.02 0.03 % Zero-bias stability 10-second smoothing, 1 σ 0.05 0.055 0.06 milligram Random Walk with Speed Allan variance 0.017 0.018 0.02 m/s/√h Orthogonality error Axis to axis 0.05 0.1 ° Data update rate 1 1000 Hertz Bandwidth 200 Hertz Parameters Test Conditions Minimum value Typical value Maximum value Unit Gyro range ±125 °/s ±250 °/s ±500 °/s ±1000 °/s ±2000 °/s ±4000 °/s Scale factor error 0.05 0.1 % Zero-bias repeatability 10-second smoothing,
1 sigma3 6 °/h Full-temperature zero-bias error -40~85℃
10-second smoothing,
1 sigma0.015 0.03 °/s Scale factor nonlinearity 0.008 0.01 % Zero-bias stability 10-second smoothing,
1 sigma3 6 °/h Random Walk in Angle Allan variance 0.13 0.15 0.175 °/√h Orthogonality error Axis to axis 0.05 0.1 ° Data update rate 1 1000 Hertz Bandwidth 200 Hertz
Chinese Chips Powering AI & New Energy Revolution
We look forward to achieving win-win cooperation with you. Please feel free to contact us for consultation and discussion, and let’s work together to create a new future for the industry.
Room 2-709, Building 1, Zijin Oriental, No. 288 Qiyue Street, Suzhou Industrial Park
