ADIS16488A Tactical Grade Ten Degrees of Freedom Inertial Sensor

Applications

The ADIS16488A iSensor® device is a complete inertial system that includes a triaxis gyroscope, a triaxis accelerometer, triaxis magnetometer, and pressure sensor. Each inertial sensor in the ADIS16488A combines industry-leading iMEMS® technology with signal conditioning that optimizes dynamic performance. The factory calibration characterizes each sensor for sensitivity, bias, alignment, and linear acceleration (gyroscope bias). As a result, each sensor has its own dynamic compensation formulas that provide accurate sensor measurements.

The ADIS16488A provides a simple, cost-effective method for integrating accurate, multiaxis inertial sensing into industrial systems, especially when compared with the complexity and investment associated with discrete designs. All necessary motion testing and calibration are part of the production process at the factory, greatly reducing system integration time. Tight orthogonal alignment simplifies inertial frame alignment in navigation systems. The SPI and register structure provide a simple interface for data collection and configuration control.

The ADIS16488A uses the same footprint and connector system as the ADIS16375, ADIS16480, and ADIS16485, which greatly simplifies the upgrade process. The ADIS16488A is packaged in a module that is approximately 47 mm × 44 mm × 14 mm and includes a standard connector interface.

Features and Benefits
  • Triaxial, digital gyroscope, ±450°/sec dynamic range
    ±0.05° orthogonal alignment error
    5.1°/hr in-run bias stability
    0.26°/√hr angular random walk
    0.01% nonlinearity
  • Triaxial, digital accelerometer, ±18 g
  • Triaxial, delta angle and delta velocity outputs
  • Triaxial, digital magnetometer, ±2.5 gauss
  • Digital pressure sensor, 300 mbar to 1100 mbar
  • Fast start-up time, ~500 ms
  • Factory-calibrated sensitivity, bias, and axial alignment
    Calibration temperature range: −40°C to +85°C
  • SPI-compatible serial interface
  • See data sheet for additional features.
Sensors
MEMS
Aerospace and Defense
  • Solutions
Software & Systems Requirements
Data Sheets
Documentnote
ADIS16488A: Tactical Grade Ten Degrees of Freedom Inertial Sensor Data Sheet (Rev. C)PDF 806 kB
Application Notes
Documentnote
AN-1295: Mechanical Design Tips for ADIS16375, ADIS16480, ADIS16485, and ADIS16488 (Rev. 0)PDF 277 kB
User Guides
Documentnote
ADIS1648x Evaluation on the EVAL-ADIS SystemWIKI
Frequently Asked Questions
Documentnote
FAQ: Gyroscope Sensitivity/Scale Factor Evaluation (EngineerZone™)
FAQ: Gyroscope In-Run Bias Stability (EngineerZone™)
FAQ: Gyroscope Noise Density (EngineerZone™)
FAQ: Gyroscope Angle Random Walk (EngineerZone™)
Order Information
Part NumberPackagePacking QtyTemp RangePrice 100-499Price 1000+RoHS
ADIS16488BMLZ ProductionMSM LAMINATEOTH 1-40 to 105C16191190E
ADIS16488CMLZ ProductionMSM LAMINATEOTH 0-55 to 105C20221520E
Evaluation Boards
Part NumberDescriptionPriceRoHS
ADIS16IMU1/PCBZBreakout Board69Y
EVAL-ADISZEvaluation Board469Y
Reference Materials
ADIS16488A: Tactical Grade Ten Degrees of Freedom Inertial Sensor Data Sheet (Rev. C) adis16488a
ADIS16488A:术级10自由度惯性传感器 (Rev. 0) adis16488a
EVAL-ADIS USB驱动程序安装文件 adis16480
EVAL-ADIS系统的IMU评估软件(版本1.9.7) (Rev. 1.16.1) adis16480
AN-1295: Mechanical Design Tips for ADIS16375, ADIS16480, ADIS16485, and ADIS16488 (Rev. 0) adis16375
AN-1295: ADIS16375、ADIS16480、ADIS16485和ADIS16488的机械设计技巧 (Rev. 0) adis16375
Sensor Fusion Approach to Precision Location and Tracking for First Responders adis16488a
Designing For Low Noise Feedback Control With Mems Gyroscopes adis16485
The Basics of MEMS IMU/Gyroscope Alignment adis16488a
MS-2694:实现新一代航空电子系统 adis16480
MEMS和FOG的精确导航之争 adis16480
INS Faceoff: MEMS vs FOGs, InsideGNSS, July/Aug 2012 adis16480