LandMark TM 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, ultra-low gyro noise, and wide sensor bandwidth.

Specifications:

Gyro Noise: 0.0016º/sec/√Hz
Accel Noise: 0.05 mg/√Hz
Sensor Bandwidth: ≥250 Hz
Gyro Bias In-Run: 3º/hour 1σ
Bias Over Temperature: < 90°/hour 1σ
Compensated Misalignment: < 0.5 mrad
g-Sensitivity: < 0.001º/sec/g 1σ
Temperature Calibration: Full (Bias & SF)
Data Format: 16/24/32-bit (selectable)
Message Rate: RS-422/485 ≤ 5 kHz (selectable)
External Sync: up to 6 kHz
CAN BUS: 2.0B 1 MHz
Vibration: 8grms
Shock: 600g
Weight: < 115 grams
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.

Export Classification: Commerce ECCN7A994 (NLR)

Connector and Pin Assignments: The IMU uses a M83513/03-BN mating connector with specific pin assignments for RS-485, power, CAN, and other functions. Unused inputs must be connected to signal ground.

Performance Parameters:

Range: ± 250°/sec, ± 490°/sec, ± 6 g’s, ± 15 g’s
Scale Factor Error: ≤ 0.1%
Non-Linearity: ≤ 0.1% of Full Scale
Alignment and G-Sensitivity: < 0.5 mrad, < 0.001°/s/g 1σ
Operating Temperature Range: -40˚C to +85˚C
Non-Operating Temperature Range: -55˚C to +85˚C
Start-up Time: < 0.3 sec
Input Power: +7 V to +36 V Max.
MTBF: 53,869 hrs (per MIL-STD-217F)

Mechanical and Environmental: The IMU is designed to withstand high vibration and shock levels, with a compact size and lightweight construction.

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 TM 60 IMU

LandMark TM 60 IMU

Catalog excerpts

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