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LandMark™60 IMU

Product catalog summary

Overview: The LandMarkTM 60 IMU is a low noise MEMS Inertial Measurement Unit (IMU) designed for various stabilization and navigation applications. It is characterized by its non-ITAR status, making it suitable for international commerce under ECCN7A994 (NLR).

Key Specifications:

Gyro Noise: Ultra-low at 0.0016º/sec/√Hz.
Accel Noise: Low at 0.05 mg/√Hz.
Sensor Bandwidth: Wide, ≥250 Hz.
Gyro Bias In-Run: 3º/hour 1σ.
Bias Over Temperature: < 90°/hour 1σ.
Compensated Misalignment: < 0.5 mrad and g-Sensitivity < 0.001°/sec/g 1σ.
Temperature Calibration: Full calibration for bias and scale factor.
Data Format: Selectable 16/24/32-bit.
Communication: RS-422/485 with message rate ≤ 5 kHz, CAN BUS 2.0B at 1 MHz.
Environmental Tolerance: Vibration at 8grms, shock at 600g.
Weight and Power: Lightweight at < 115 grams and low power consumption < 500 mW typical.

Applications: The IMU is suitable for airborne platform stabilization, antenna stabilization and pointing, EO/IR stabilization, LIDAR stabilization, navigation, and flight testing.

Technical Details:

Connector: M83513/03-BN with specific pin assignments for RS-485, power, and CAN communication.
Outputs: Includes roll, pitch, yaw gyros, accelerometers, and temperature with typical accuracy of ± 0.5°C.
Parameter Ranges: Gyro range of ± 250°/sec and ± 490°/sec, accelerometer range of ± 6 g’s and ± 15 g’s.
Scale Factor Error: 0.05% to 0.1% of full scale.
Operating Conditions: Temperature range from -40˚C to +85˚C, with start-up time < 0.3 sec.
MTBF: 53,869 hours based on MIL-STD-217F, Notice 2.

Additional Notes: The IMU includes a self-test feature and requires unused inputs to be connected to signal ground. The specification is subject to change without notice.

Catalog excerpts

Automated Testing Comprehensive ERP Environmental Test Lab: - Shock - Vibration - Temperature Calibration - G-Sensivity -Axis Alignment - Centrifuge - GPS Simulation Products: Gyros Accelerometers IMU VG AHRS VG/GPS G PS/AH RS INS/GPS NON-ITAR MEMS IMU Ultra Low Gyro Noise 0.0016°/sec/lHz Low Accel Noise 0.05 mg/lHz Wide Sensor Bandwidth >250 Hz Gyro Bias In-Run 3°/hour 1o Bias Over Temperature <90°/hour 1o Compensated Misalignment < 0.5 mrad and g-Sensitivity < 0.001 °/sec/g 1o Full Temperature Calibration (Bias & SF) 16/24/32-bit Data Format (selectable) RS-422/485 Message Rate < 5 kHz (selectable) External Sync up to 6 kHz CAN BUS 2.0B 1 MHz Vibration 8grms Shock 600g Light Weight < 115 grams Low Power < 500 mW typical Gladiator Technologies Division LKD Aerospace 8020 Bracken Place SE Applications Airborne Platform Stabilization Antenna Stabilization Antenna Pointing EO/IR Stabilization LIDAR Stabilization Navigation Flight Testing o®$o [email protected] www.gladiatortechnologies.com

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Axes (Top View) Right Hand Rule Specification Mating Connector: M83513/03-BN Pin No. Note: Any unused inputs (Pins 4, 6, 9) must be connected to signal ground (Pin 8). Specification subject to change without notice

Open the catalog to page 2

LandMark™60 IMU

LandMark™60 IMU

Catalog excerpts

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