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Ultra High Accuracy Gyro Theodolite

Ultra High Accuracy Gyro Theodolite

ER-GT-02 (≤3.6") Features:
1. Orienteering accuracy ≤3.6" (1σ);
2. Pit interference ability is strong, integrated fuselage design, compact structure, stable performance;
3. Has the functions of low lock, automatic zero observation and etc.

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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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