Attribute | Value |
---|---|
Measuring range | ±450°/s |
Bias instability | 0.3°/h |
Random walk | 0.15º/√h |
Scale factor repeatability | 100ppm |
Bandwidth (-3dB) | 250Hz |
Accelerometer Range | ±20g |
Accelerometer bias stability | 0.07mg |
Voltage | 3.3V |
The ADIS16488HA Inertial Measurement Unit (IMU) represents a cutting-edge inertial sensing solution, integrating tri-axis gyroscope and accelerometer functionality into a unified, high-performance system. Engineered for precise measurement of three-dimensional angular velocities, linear accelerations, and derived dynamic parameters, this IMU delivers mission-critical accuracy through advanced error mitigation algorithms.
Parameter | Test Conditions | Min | Typical | Max | Unit |
---|---|---|---|---|---|
Gyroscope Dynamic Range | ±450 | º/s | |||
Zero-bias Instability | Allan variance | 0.3 | º/h | ||
Zero Bias Stability | 10s smooth, RMS | 3 | º/h | ||
Random Walk | 1σ | 0.15 | º/√h | ||
Scale Factor Repeatability | 1σ | 100 | ppm | ||
Bandwidth (-3dB) | 250 | Hz | |||
Accelerometer Dynamic Range | ±20 | g | |||
Accelerometer Zero Bias Stability | Allan variance | 0.07 | mg | ||
Voltage | Direct current | 3.3 | V | ||
Operating Temperature | -45 | 85 | ℃ |
Note: Specifications subject to change without notice. Contact our technical team for application-specific performance verification.