MSG3000D Tri-axis MEMS Gyros

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  1. Based on MEMS Process
  2. Angular Rate, Temp. Output
  3. 2000g Shock Resistance
  4. High-density, 3 Axis Integration
  5. RS422 Interface
  6. Compact, Higher Reliability

Description

MSG3000D Tri-axis MEMS Gyros – MEMS Inertial Devices and Systems

Applications

  • Inertial Navigation: Inertial Guidance, Integrated Navigation, Platform Stabilization
  • Short-term Navigation: Flight Control, Ballistic Correction, Telemetry
  • Posture Control: UAV (Unmanned Aerial vehicle), Antenna Orientation, North Finder
  • Automotive: Balance Measurement

 

Parameter Unit MSG3000D
Range °/s X: ±250 Y: ±250 Z: ±250
Scale Factor Non-linearity ppm 500 500 500
Scale Factor Repeatability ppm
Scale Factor Temp. Coefficient ppm/°C
Short-term Bias StabOty (1o) °/h 35 35 35
Bias Repeatability °/h 35 35 35
Bias Temp. Coefficient °/s/°C
Threshold °/s 0.01 0.01 0.01
Resolution °/s 0.01 0.01 0.01
Random Walk °/√h
Start Up Time s 2 2 2
Bandwidth Hz 250
Power Consumption mW ≤ 500
Output RS422
Package Metal Package
Operating Temp. °C -40~+85
Storaging Temp. °C -55~+100
Shock Resistance g 2000
All values are typical at +25V5VDC unless otherwise statement.

 

Structure (unit: mm)