YYDS-488

Manufacturer:: Shenzhen Senseiot

SENSEIOT YYDS-488 Military-Grade 10-Axis IMU Inertial Measurement Unit

Specifications

Product Introduction

The YYDS488 is a high-performance inertial measurement unit designed for precision motion sensing applications. It offers superior stability and accuracy compared to industry-standard reference models, making it ideal for demanding navigation and control systems.

Features

  • Low bias instability for both gyroscope and accelerometer
  • Excellent angular random walk performance
  • Minimal scale factor error across full range
  • Stable operation over wide temperature range
  • High output data rate for real-time applications

Applications

  • Precision navigation and guidance systems
  • Stabilized platforms and gimbals
  • Autonomous vehicles and robotics
  • Aerospace and defense systems
  • Industrial motion control

Specifications Table

Parameter Value
Gyroscope Dynamic Range 500 deg/s
Accelerometer Dynamic Range 16 g
Output Data Rate (ODR) 200 Hz
Gyroscope Bias Instability (@Allan) 0.42 deg/h (X), 0.403 deg/h (Y), 0.361 deg/h (Z)
Gyroscope Bias Stability (@10s smooth, 1 sigma) 1.5230 deg/h (X), 1.5556 deg/h (Y), 1.3971 deg/h (Z)
Gyroscope Angular Random Walk (@1 sigma) 0.0606 deg/√h (X), 0.0626 deg/√h (Y), 0.0468 deg/√h (Z)
Gyroscope Bias Temperature Coefficient (@-40~85℃) 0.000336 deg/s/°C (X), 0.000374 deg/s/°C (Y), 0.000184 deg/s/°C (Z)
Gyroscope Scale Factor Error (@FullScale) 43 ppm (X), 150 ppm (Y), 74 ppm (Z)
Accelerometer Bias Instability (@Allan) 5.2030 ug (X), 5.6297 ug (Y), 5.3453 ug (Z)
Accelerometer Bias Stability (@10s smooth, 1 sigma) 13.6905 ug (X), 13.4632 ug (Y), 14.8722 ug (Z)
Accelerometer Velocity Random Walk (@1 sigma) 0.0063 m/s/√h (X), 0.0065 m/s/√h (Y), 0.0073 m/s/√h (Z)
Accelerometer Bias Temperature Coefficient (@-40~85℃) 0.006837 mg/°C (X), 0.010502 mg/°C (Y), 0.009852 mg/°C (Z)

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Datasheet: