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

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

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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
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
Parameter Test Conditions Min Typical Max Unit
Gyroscope
Dynamic measuring range ±450 º/s
Zero-bias instability Allan variance, better than 0.3 º/h
Zero bias stability 10s smooth, RMS, better than 3 º/h
Zero bias in full temperature range -40℃ ~ 85℃, 10 s smooth, rms 20 º/h
Random walk 1σ 0.15 º/√h
Zero-bias repeatability 1σ 5 º/h
Scale factor repeatability 1σ 100 ppm
Scale factor nonlinearity 1σ 100 ppm
Bandwidth (-3dB) 250 Hz
Cross coupling 0.1 %
Resolution 2 º/h
Acceleration sensitivity 2 °/h/g
Accelerometer
Dynamic measuring range ±20 g
Zero bias stability Allan variance 0.07 mg
Zero bias in full temperature range -40℃ ~ 85℃, 10 s smooth, rms 3 mg
Zero bias stability 10s smooth, RMS, better than 0.25 mg
Random walk 1σ 0.029 m/s/√h
Zero-bias repeatability 1σ 0.5 mg
Scale factor repeatability 1σ 500 ppm
Scale factor nonlinearity FS=20g 500 ppm
Bandwidth (-3dB) 250 Hz
Cross coupling 0.1 %
Electrical Characteristics
Voltage Direct current 3.3 V
Power consumption 1.5 1.5 W
Ripple P-P 48±2 100 mV
Environmental Specifications
Operating temperature -45 85 ℃
Storage temperature -55 85 ℃
Product Diagrams
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 ADIS16488 Inertial Sensor Tactical Grade 10‑DOF MEMS Inertial Measurement Unit for INS

Product Tags:

ADIS16488 Inertial Measurement Unit

      

Tactical Grade Inertial Measurement Unit

      

10‑DOF MEMS Inertial Measurement Unit

      
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