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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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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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High Precision Directional Sensor

High Precision Fluxgate Directional Assembly

ER-OS-07 (±0.1°) Features:
1. Temperature: -40℃~150℃;
2. Accurate measurement under strong vibration environment with 16g peak value (20Hz~100Hz);
3. Shock resistance 1000g, vibration resistance 20grms;
4. Digital data transmission;
5. With minimum size of Φ31mm×384mm (customized to different needs).

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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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