MSG1100D MEMS Gyros

  1. Based on MEMS Process
  2. Angular Rate & Temp. Output
  3. 2000g Shock Resistance
  4. Integrate Signal Conditioning
  5. SPI/RS422 Interface
  6. Self-Test

Description

MSG1100D 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 MSG1100D-300 MSG1100D-500
Range °/s ±300 ±500
Scale Factor Nonlinearity %FS 0.03 0.05
Scale Factor Repeatability ppm 200 500
Scale Factor Temp. Coefficient ppm/°C 40 60
Short-term Bias Stability (1 σ) °/h 10 20
Bias Repeatability °/h 10 20
Bias Temp. Coefficient °/s/°C 0.001 0.002
Threshold °/s 0.005 0.01
Resolution °/s 0.005 0.01
Random Walk °/√h 0.15 0.30
Start up time s 1 1
Bandwidth Hz Typical:62

Optional: 125,250,500

Typical:62

Optional: 125,250,500

Power Consumption mW 125 125
Interface SPI/RS422 SPI/RS422
Packaging Titanium Alloy Titanium Alloy
Operating Temp. °C -40~+85 -40~+85
Storage Temp. °C -55~+100 -55~+100
Shock Resistance g 2000 2000
All values are typical at +25°C.+5Vdc unless otherwise statement.

Structure (unit: mm)