Navigation & Inertial Sensing

Tactical Grade

SDC500 MEMS Inertial Measurement Unit (IMU) (License Free)

Ideal for High-Precision Commercial & Industrial Applications

Systron Donner Quartz MEMS
The compact SDC500 Quartz MEMS Inertial Measurement Unit (IMU) meets commercial aerospace, industrial and marine application needs globally. It is available in several performance-cost options ranging in accuracy from precision 1°/hr gyro and 1 mg accelerometer to 20°/hr gyro and 5 mg accelerometer bias over temperature, shock, and vibration environments. This enables customers to select the SDC500 version that meets their specific performance and budget requirements from near tactical grade to high-performance commercial/industrial grade. The SDC500 IMU is constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The SDC500’s breakthrough gyro design retains Quartz MEMS sensitivity and linearity and greatly improves noise immunity.

The small, light, low-power, hermetically sealed SDC500 IMU provides industry-standard serial communication, configurable communications protocols, Time of Validity (TOV) sync, continuous Built-in Test (BIT), electromagnetic interference (EMI) protection, long MTBF and flexible input power compatibility making the SDC500 IMU easy to use in a wide range of challenging applications and operating environments.

PARAMETERS GYRO CHANNELS ACCELERATION CHANNELS
Bias (Over Temperature) 1°/hr - 20°/hr 1.0 mg - 5.0 mg
Bias In-Run Stability 1.0°/hr - 5.0°/hr 150 μg - 400 μg
Random Walk Noise 0.02°/√hr - 0.04°/√hr 100 μg /√Hz - 200 μg /√Hz
Operating Temperature -40 °C to +71 °C -41 °C to +71 °C
Vibration (Operating) 12g - 8g rms 12g - 8g rms

Features

  • 1 to 20°/hr Gyro Bias Over Temperature
  • 19 in.3 Compact Size
  • 12 g rms, Vibration Operating Performance Environment (20-2,000 Hz random)
  • Mature, Reliable, Proven Performance & Superior Quality
  • Greater Than 100,000 hr MTBF
  • Data Time of Validity (TOV) Input & Output Synchronization
  • Smaller, Lower Power, and Cost-Effective Replacement for Open-Loop FOG IMU

Applications

  • General Aviation / Flight Control
  • AHRS (Attitude Heading Reference System)
  • GPS-aided Navigation
  • Autonomous and Remotely Operated Vehicles
  • Aerial and Marine Geo-mapping / Surveying
  • Commercial Pipeline Inspection
  • Mining / Agriculture
  • Robotics