MEMS Inertial Navigation System

North Seeker
- FOG North Seeker
- MEMS North Seeker
Gyro Sensor
- Ring Laser Gyroscope
- DTG
- Fiber Optic Gyroscope (FOG)
- MEMS Gyroscope
- Liquid Floated Gyro
Accelerometer
- Quartz Accelerometer
- MEMS Accelerometer
- VF/ IF Conversion Circuit
IMU
- MEMS IMU
- FOG IMU
INS
- FOG Inertial Navigation System
- MEMS Inertial Navigation System
- DTG Inertial Navigation System
AHRS
Positioning & Orientation System
Logging Tool/Gyro Tool
- SingleShot & MultiShot Logging Tool
- Measurement While Drilling (MWD)
- FOG Continuous Gyro Tool
- Fluxgate Directional Assembly
- FOG Directional Assembly
- MEMS Directional Assembly
- FOG Directional Sensor
- MEMS Directional Sensor
- Quartz Presure Sensor
- High-Temp Quartz Accelerometer
- Calibration Device
Inertial Geodetic Survey System
Gyrocompass
- Fiber Optic Gyro Compass
Gyro Theodolite
Inertial Testing Device
GNSS Chip
GNSS Board
GNSS Module
GNSS Antenna
Satellite Receiver
Satellite Handheld Device
Satellite Signal Simulator
Anti UAV Defence System
Electrical Motor
- Civil Motor
- Industrial Motor
Integrated Circuit
- DSP
- CPU
Pressure Sensors
Tilt Sensor
- Routine Tilt Sensor (Single Axis)
- Dynamic Tilt Sensor (Dual Axis)
- Wireless Transmission Tilt Sensor
- Digital Display Tilt Sensor
- Single Board of Tilt Sensor
- Tilt Switch
- Angle Sensor
Digital Compass
Acceleration Sensor
Power Supply
Robot Joint Reducer
Industrial Intelligentization System

Ericco provides high accuracy and low cost MEMS Inertial Navigation System (INS), inertial positioning system, inertial orientation system to the customers worldwide, the quality and after service are proven to be well guaranteed. Ericco also customizes various based MEMS inertial navigation/positioning/orientation system according to the customers' special requirements. Just come and get more details with us.

Mapping-level & Ultra-precision GNSS/MEMS INS

ER-GNSS/MINS-01:
1. Delivers extremely accurate navigation information: 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. Delivers accurate navigation information: 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. Delivers accurate navigation information: 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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Integrated Navigation System

ER-MINS-5610 (0.1°) Features:
1. Equipped with MEMS gyroscope and accelerometer and mapping multi-mode multi-frequency GNSS receiver;
2. It can achieve a single antenna dynamic alignment or dual antenna-assisted fast high-precision orientation;
3. The directional accuracy can reach up to 0.1 deg.

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MEMS Integrated Navigation System

ER-MINS-5651 (0.1°) Features:
1. Equipped with MEMS gyroscope and accelerometer and mapping multi-mode multi-frequency GNSS receiver;
2. It can achieve a single antenna dynamic alignment or dual antenna-assisted fast high-precision orientation;
3. The directional accuracy can reach up to 0.1 deg.

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