2-Axis North-Seeking MEMS Gyro
ER-2MG-051
1. OEM;
2. Bias Instability (1σ 25℃): 0.01~0.02º/h;
3. Light Weight.
ER-2MG-051
1. OEM;
2. Bias Instability (1σ 25℃): 0.01~0.02º/h;
3. Light Weight.
ER-2MG-052
1. OEM;
2. Bias Instability: 0.03º/h;
3. Light Weight.
ER-2MG-053
1. OEM;
2. Bias Instability (1σ 25℃): 0.3-0.1º/h;
3. Light Weight.
ER-2MG-054
1. OEM;
2. Bias Instability (1σ 25℃): 1º/h;
3. Small Volume.
ER-2MG-061
1. Smallest Size;
2. Bias Instability(1σ 25℃): 0.01-0.02º/h;
3. Light Weight.
ER-2MG-062
1. Smallest Size;
2. Bias Instability(1σ 25℃): 0.03º/h;
3. Light Weight.
ER-2MG-063
1. Bias Instability(1σ 25℃): 0.3-0.1º/h;
2. Smallest Size;
3. Light Weight.
ER-2MG-064
1. Smallest Size;
2. Bias Instability (1σ 25℃): 1º/h;
3. Light Weight.
ER-2MG-091
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.01-0.02º/h;
3. Size: 120mm x Φ30mm.
ER-2MG-092
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.03º/h;
3. Size: 120mm x Φ30mm
ER-2MG-093
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.3-0.1º/h;
3. Size: 120mm x Φ30mm.
ER-2MG-094
1. Cylinder;
2. Bias Instability (1σ 25℃): 1º/h;
3. Size: 120mm x Φ30mm.
ER-2MG-101
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
ER-2MG-102
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
ER-2MG-103
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
ER-2MG-104
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
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.
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°.
ER-FINS-40:
1. Highly reliable and extremely accurate fiber optic gyroscopes;
2. Large range and high precision quartz accelerometers;
3. Built-in full-band full-system dual-antenna positioning and orientation GNSS module.
ER-FIMU-40:
1. All solid-state three-axis fiber optic gyroscope;
2. High reliability;
3. Three-axis quartz flexible accelerometers.
ER-FOG-851 (≤0.05~0.1º/h)
1. Bias stability: 0.05~0.1º/h;
2. 78.5×78.5×35mm;
3. Suitable for flight control platform.
ER-FNS-01D
1.Internal shock absorber, can adapt to large impact and vibration;
2.30s fast alignment, azimuth accuracy 1°; 90s accurate alignment, azimuth accuracy 0.5°;
3.Dynamic north finding, accurate north finding and attitude following in the case of vibration;
ER-FNS-02 (0.02°-0.1°):
1. High precision initial alignment & direction control solution;
2. FOG and quartz accelerometer as core sensors;
3. High stability and reliability.
ER-FNS-03 (0.5°-1°):
1. Low cost FOG north seeking solution;
2. Specially suitable for mining application;
3. 3-axis FOG & 3-axis accelerometer.