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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.

Er Gnssmins 01 Mapping Level & Ultra Precision Gnss Mems Ins

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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Er Gnssmins 03 High Precision Mems Integrated Navigation System.

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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Er Gnssmins 05 Cost Efficient Gnss Aided Mems Ins.

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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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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Integrated Navigation System

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

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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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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MEMS Inertial Navigation System

MEMS Inertial Navigation System

ER-MINS-210/230 (0.3~1.0°) Features:
1. Provide horizontal attitude, heading attitude, longitude, latitude, altitude, etc;
2. Can be widely used in unmanned aerial vehicles, vehicle navigation, aviation and platform stability control and other fields.

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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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MEMS Integrated INS

MEMS Integrated INS

ER-MINS-5680 (0.5°) Features:
1. 0.1° (dynamic alignment);
2. 0.5° (low dynamic dual antenna assistance, 2m baseline);
3. Support fast and high precision orientation up to 0.1 °.

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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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