MSG9000D MEMS Gyros

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  1. Based on MEMS Process
  2. Standard Ceramic Packaging
  3. Ultra-Small Size
  4. Low Power
  5. +5V Voltage Input
  6. SPI Interface
  7. Output
  8. Excellent Environmental Adaptability

Description

MSG9000D 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 MSG9000D-300
Range °/s ±300 (±50~±7200Adjustable)
Scale Factor Non-linearity %FS 0.03
Scale Factor Repeatability: ppm 200
Scale Factor Temp. Coefficient ppm/°C 40
Short-term Bias Stability (1 σ): °/h 10
Bias Repeatability °/h 10
Bias Instability (Allan variance) °/h 1
Random Walk °/√h 0.15
Threshold/Resolution °/s 0.005
Bias Temp. Coefficient °/s/°C 0.001
Start Up Time s 1
Bandwidth Hz 62 (125, 250 Adjustable)
Power Consumption mW 125
Shock Resistance g 2000
Operating Temp. °C -40~+85
Storage Temp. °C -55~+100
Output SPI
Package LCC20 Ceramic Packaging
All values are typical at +25°C, +5Vdc, unless otherwise statement.

 

Structure (unit: mm)