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ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS

Categories IMU Accelerometer Gyro
Brand Name: Firepower
Model Number: 16488HA
Place of Origin: China
MOQ: 1
Price: 2000$
Payment Terms: L/C,D/A,D/P,T/T,Western Union
Supply Ability: 500/month
Delivery Time: 1 Week for sample
Packaging Details: BOX+Sponge
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
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ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS

ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS
Key Specifications
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
Product Overview

The ADIS16488HA Inertial Measurement Unit (IMU) is a complete inertial sensing solution that combines a three-axis gyroscope and three-axis accelerometer in a compact package. This tactical-grade MEMS IMU precisely measures three-axis angular rates, linear accelerations, and dynamic parameters with advanced error compensation for high-accuracy data output.

Core Features
  • Comprehensive Motion Sensing: Simultaneously captures 3D angular velocity (gyroscopes) and acceleration (accelerometers) for complete motion tracking
  • Advanced Error Compensation: Implements temperature drift compensation, mounting misalignment calibration, and nonlinearity correction to minimize systematic errors
  • Digital Interface: Provides compensated data through industry-standard SPI communication protocol for easy system integration
Ideal for demanding applications including autonomous vehicles, robotics, and aerospace systems, the ADIS16488HA delivers reliable performance for inertial navigation and attitude control through its integrated hardware and intelligent error mitigation.
Technical Specifications
ParameterTest ConditionsMinTypicalMaxUnit
Gyroscope
Dynamic measuring range±450º/s
Zero-bias instabilityAllan variance, better than0.3º/h
Zero bias stability10s smooth, RMS, better than3º/h
Zero bias in full temperature range-40℃ ~ 85℃, 10 s smooth, rms20º/h
Random walk0.15º/√h
Zero-bias repeatability5º/h
Scale factor repeatability100ppm
Scale factor nonlinearity100ppm
Bandwidth (-3dB)250Hz
Cross coupling0.1%
Resolution2º/h
Acceleration sensitivity2°/h/g
Accelerometer
Dynamic measuring range±20g
Zero bias stabilityAllan variance0.07mg
Zero bias in full temperature range-40℃ ~ 85℃, 10 s smooth, rms3mg
Zero bias stability10s smooth, RMS, better than0.25mg
Random walk0.029m/s/√h
Zero-bias repeatability0.5mg
Scale factor repeatability500ppm
Scale factor nonlinearityFS=20g500ppm
Bandwidth (-3dB)250Hz
Cross coupling0.1%
Electrical Characteristics
VoltageDirect current3.3V
Power consumption1.51.5W
RippleP-P48±2100mV
Environmental Specifications
Operating temperature-4585
Storage temperature-5585
Product Diagrams
ADIS16488 IMU structural diagram showing component layout ADIS16488 IMU dimensional drawing with measurement specifications ADIS16488 IMU interface and connection diagram
Quality ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS for sale
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