Low Cost Fiber Optic Gyroscope
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-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-GNSS/MINS-01:
1. High reliability and high precision;
2. Built-in full-band full-system dual-antenna positioning and orientation GNSS module;
3. Provide extremely accurate integrated navigation information.
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.
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-MNS-05/05Mini (0.25°-1°):
1. New mini version: 40*40*42mm(with shell)/27*26*34(without shell and baseboard);
2. The inner platform body adopts the design of China Ding, with high reliability;
3. Shock and vibration resistance, resistant to harsh environment.
ER-MNS-06 (0.25°-1°):
1. Smallest Volume MEMS north seeker in the world;
2. Resistant to harsh environment;
3. Light weight, low power consumption.
ER-MNS-09(0.25°-1°):
1. Special-shaped design: adopts a cylindrical design (120mm x Φ30mm);
2. High precision pointing: with a north-seeking accuracy up to 0.25°secψ(1σ);
3. Low power consumption, MAX endurance.
ER-MNS-10 (0.25°-1°):
1. The thinnest and lightest MEMS north seeker (40g);
2. High-precision MEMS gyroscopes and accelerometers;
3. High stability and reliability.
ER-MIMU-01/01Mini
1. New mini version: 40*40*42mm(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Can find north independently.
ER-MIMU-02/02Mini
1. New mini version: 40*40*42mm(with shell)/27*26*34(without shell and baseboard);
2. The inner platform body adopts the design of China Ding, with high reliability;
3. Gyro bias instability(1σ 25℃): 0.03~0.05deg/hr.
ER-MIMU-03/03Mini
1. New mini version: 40*40*42mm(with shell)/27*26*34(without shell and baseboard);
2. OEM modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): <0.3~0.1deg/hr.
ER-MIMU-04/04Mini
1. New mini version: 40*40*42mm(with shell)/27*26*34(without shell and baseboard);
2. -40~80°C temperature compensation;
3. OEM modular design, strong applicability.
ER-MIMU-05
1. Smallest volume: 38.6mm x 44.8mm x25.5mm;
2. Range can be selected;
3. Light weight: ≤70g.
ER-MIMU-06
1. Smallest volume: 38.6mm x 44.8mm x25.5mm;
2. Light weight: ≤70g;
3. Temperature compensation: -40℃~ + 80℃.
ER-MIMU-07
1. Smallest volume: 38.6mm x 44.8mm x25.5mm;
2. Light weight: ≤70g;
3. Temperature compensation: -40℃~ + 80℃.
ER-MIMU-08
1. Smallest volume: 38.6mm x 44.8mm x25.5mm;
2. Light weight: ≤70g;
3. Temperature compensation: -40℃~ + 80℃.
ER-2MG-01/01mini
1. OEM;
2. Bias Instability (1σ 25℃): 0.01~0.02º/h;
3. Light Weight.
ER-2MG-02/02mini
1. OEM;
2. Bias Instability: 0.03-0.05º/h;
3. Light Weight.
ER-2MG-03/03mini
1. OEM;
2. Bias Instability (1σ 25℃): 0.3-0.1º/h;
3. Light Weight.
ER-2MG-04/04mini
1. OEM;
2. Bias Instability (1σ 25℃): 1º/h;
3. Small Volume.
ER-2MG-05
1. Smallest Size;
2. Bias Instability(1σ 25℃): 0.01-0.02º/h;
3. Light Weight.
ER-2MG-06
1. Smallest Size;
2. Bias Instability(1σ 25℃): 0.03-0.05º/h;
3. Light Weight.
ER-2MG-07
1. Bias Instability(1σ 25℃): 0.3-0.1º/h;
2. Smallest Size;
3. Light Weight.
ER-FNS-01 (0.02°-0.5°):
1. Dynamic direction initial alignment & keeping solution;
2. Suitable for land surveying and mapping & direction control for moving vehicles, carriers;
3. High performance FOG & Quartz accelerometer as core sensor.