MSG7100D MEMS Gyros

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  1. Based on MEMS Process
  2. Standard Ceramic Packaging
  3. Ultra-Small Size
  4. Low Power
  5. SPI Interface
  6. Self-Test
  7. Output
  8. 2000g Shock Resistance

Description

MSG7100D 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 MSG7100D-300
Range °/s ±300(±100~±5000)
Scale Factor Nonlinearity %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

Typical:62

Optional: 125,250,500

Power Consumption mW 125
Shock Resistance g 2000
All values are typical at +25 °C, +5Vdc unless otherwise statement

 

Structure (unit: mm)