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 Integrated Navigation System

High-precision 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

Cost-efficient GNSS aided MEMS INS

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 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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High Performance FOG INS

High Performance FOG INS

ER-FINS-98 (0.1°secψ):
1. Azimuth accuracy ≤ 0.1° secψ (1σ);
2. Attitude accuracy ≤ 0.02° (1σ);
3. Azimuth holding accuracy ≤ 0.05°sec lat (1σ).

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High Precision FOG INS

High Precision FOG INS

ER-FINS-120 (0.02°):
1. Heading accuracy (1σ): ≤0.02°;
2. Attitude accuracy (1σ): ≤0.02°;
3. Positional accuracy (1σ): 1.0nm/2h.

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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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