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The all new LandMark™10 VG builds upon the extensive LandMark™10 IMU and AHRS product lineage and is now offered with a substantially improved upgrade employing our latest low noise gyro (0.014°sec/√Hz) technology for improved bias and with improved environmental sealing and MIL-SPEC connector. It provides internally temperature compensated RS485 output of delta velocity and delta theta as well as VG pitch and roll angle outputs. This VG is ideal for appli-cations requiring low cost, ultra low power consumption, rugged packaging, small size, light weight and no inherent wear out modes for long life. The signature feature of the unit is the accurate pitch & roll angle performance, which is optimized with fully temperature compensated bias and scale factor, compensated misalignment and g-sensitivity.

Download LandMark™10 Vertical Gyro Datasheet

Key Features:

• Low Cost & Rugged Vertical Gyro

• Vertical Gyro (No Magnetometers) ~ Pitch & Roll Angles ±0.25° stationary

• Low Gyro Noise <0.014°/sec/√Hz 1σ

• Low Accel Noise <0.05mg/√Hz 1σ

• In Run Gyro Bias 25° /hour 1σ

• Fully Temperature Compensated Bias and Scale Factor

• Compensated Misalignment 1mrad and g-Sensitivity <0.03°/sec/g 1σ

• Low Power 300 mW typical

• Low Voltage +3.1 to +5.5V (single sided)

• Light Weight <102 grams • Small Size < 72cm³/4.4in³

• Wide Sensor Bandwidth 140 Hz

• Bandwidth Filtering Capability

• RS485 Output 100 Hz (user selectable)

• External Sync Input (1 kHz or 1pps)

• Internal Vibration Isolation

• Precision Alignment

• 3 Internal Temperature Sensors

• Self Test & Shock Resistant

• Export Classification: ECCN7A994

The unit is highly durable and employs an FEA designed internal vibration isolator that can withstand environmental vibration and shock typically associated with commercial aircraft requirements. LandMark™ VG's include built-in firmware to accept external velocity as well as an external sync input 1 kHz (or 1pps indication). This VG is well suited for low cost flight control, land vehicle stabilization, platform and antenna stabilization, general aviation as well as laboratory use where low gyro noise, small size, low power, light weight and low cost are required.