MSG2004 Dual-axis MEMS Gyros

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  1. Based on MEMS Process
  2. Ultra-Small Size
  3. Standard Ceramic Packaging
  4. Lower Power
  5. Output
  6. 2000g Shock Resistance

Description

MSG2004 Dual-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 MSG2004
Range °/s ±250
Bias (Full Temp.) °/s <0.05
Bias Stability °/h <25
Bias Repeatability °/h <25
Nonorthogonality <3
Bias Temp. Coefficient °/s/°C <0.0005
Bandwidth Hz 100 (2~400Hz Adjustable)
Scale Factor Sensitivity ppm <200
Non-linearity:
Resolution °/s 0.005
Scale Factor Sensitivity Temp. ppm/°C <10

 

Structure (unit: mm)