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Er Mimu 01

North-Seeking MEMS IMU

ER-MIMU-01
1.  3 axis gyroscope & 3-axis accelerometer;
2. Gyro bias instability:<0.02 deg/hr;
3. Gyro bias stability (10s 1σ): <0.1 deg/hr;
4. Gyro angular random walk:<0.005 °/√h.

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Mapping Level & Ultra Precision Gnss Mems Ins

Mapping-level & Ultra-precision GNSS/MEMS INS

ER-GNSS/MINS-01:
1. Attitude accuracy: 0.01° (0.004° post-processing), heading accuracy: 0.05° (0.01° post-processing).
2. Built-in full-band full-system dual-antenna positioning and orientation GNSS module.
3. MEMS gyroscope (bias instability <0.02°/h) and MEMS accelerometer (±60g, zero bias instability <2μg)

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High-precision MEMS Integrated Navigation System

ER-GNSS/MINS-03:
1. Attitude accuracy : 0.02° (0.01° post-processing), heading accuracy: 0.05° (0.01° post-processing).
2. Built-in full-band full-system dual-antenna positioning and orientation GNSS module.
3. Suitable for applications in aviation, land, marine, and more.

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Cost-efficient GNSS aided MEMS INS

ER-GNSS/MINS-05:
1. Attitude accuracy: 0.1° (0.03° post-processing), heading accuracy: 0.1° (0.05° post-processing).
2. Built-in full-band full-system dual-antenna positioning and orientation GNSS module.
3. Variety of data interface, support RS422/RS232 and CAN.

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High Performance Dynamic FOG North Seeker

High Performance Dynamic FOG North Seeker

ER-FNS-01 (0.02°-0.5°):
1. Dynamic direction initial alignment & keeping solution;
2. Suitable for land surveying and mapping & direction control for moving vehicles, carriers;
3. High performance FOG & Quartz accelerometer as core sensor.

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