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Ericco Inertial Technology

INS

Ericco not only provides high precision and low cost FOG/MEMS/DTG inertial navigation system (INS), inertial guidance system, inertial orientation system, inertial positioning system to the customers worldwide, but also customizes various inertial navigation system. The quality and after service are proven to be well guaranteed.

High Precision Mems Inertial Navigation System

High-precision MEMS Inertial Navigation System

ER-MINS-01
1.High reliability and high precision MEMS gyroscope (bias instability <0.02°/h) and large range high precision MEMS accelerometer (±60g, bias instability <2ug).
2.The working temperature is -40℃~+80℃, and the temperature compensation of the gyroscope and accelerometer is carried out in the working temperature range, which has better bias performance.
3.It can be externally connected to satellites, odometers, barometers, etc.

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High Precision Mems Inertial Navigation System

MEMS Inertial Navigation System

ER-MINS-02
1.High reliability and high precision MEMS gyroscope (bias instability <0.02°/h) and large range high precision MEMS accelerometer (±60g, bias instability <2ug).
2.The working temperature is -40℃~+80℃, and the temperature compensation of the gyroscope and accelerometer is carried out in the working temperature range, which has better bias performance.
3.It can be externally connected to satellites, odometers, barometers, etc.

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High Precision Mems Inertial Navigation System

High-reliability Inertial Navigation System

ER-MINS-03
1.High reliability and high precision MEMS gyroscope (bias instability <0.03°/h) and large range high precision MEMS accelerometer (±60g, bias instability <2ug).
2.The working temperature is -40℃~+80℃, and the temperature compensation of the gyroscope and accelerometer is carried out in the working temperature range, which has better bias performance.
3.It can be externally connected to satellites, odometers, barometers, etc.

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High Precision Mems Integrated Navigation System

Cost-effective MEMS Integrated Navigation System

ER-GNSS/MINS-03:
1. High reliability and high precision MEMS gyroscope and MEMS accelerometer;
2. Built-in full-band full-system dual-antenna positioning and orientation GNSS module;
3. Precision aluminum alloy shell,  can be widely used in land, aviation, navigation.

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Cost Efficient Gnss Aided Mems Ins

Low-cost MEMS Integrated Navigation System

ER-GNSS/MINS-05:
1. High reliability and low cost MEMS gyroscope and accelerometer;
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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Low Cost Single Antenna Mems Ins

Low Cost Single Antenna MEMS Integrated Navigation System

ER-GNSS/MINS-07
1.High reliability and low cost MEMS IMU. The working temperature is -40℃~+80℃.
2.Built-in dual-band full-system single-antenna positioning GNSS module, supporting single-antenna high-precision positioning and velocity measurement.
3.The system can provide accurate integrated navigation information, attitude up to 0.1°, heading 0.1°.

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Low Cost FOG INS

Low Cost FOG INS

ER-FINS-70 (0.3°):
1. Heading accuracy (1σ): ≤0.3°;
2. Attitude accuracy (1σ): ≤0.03°;
3. High performance & low cost.

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Dynamically Tuned Inertial Navigation System

Dynamically Tuned Inertial Navigation System

ER-DINS-1 (0.4~0.5°) Features:
1. Strapdown inertial navigation system determination of aircraft position, heading, altitude;
2. System with emergency rapid alignment, normal alignment, navigation, correction, parameter calibration, testing, parameter binding, non volatile storage.

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