Ultra-Small Size OEM 2-Axis North-Seeking MEMS Gyro
ER-2MG-041
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Can find north independently.
ER-2MG-041
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Can find north independently.
ER-2MG-042
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): 0.03deg/hr.
ER-2MG-043
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): <0.1deg/hr.
ER-2MG-044
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. -45~85°C temperature compensation.
ER-Gyro-15
1. Using the latest three-axis MEMS gyroscope, three-axis MEMS plus strapdown inertial measurement technology;
2. Subvert the size of the traditional gyroscope tool, small to the extreme, only 30mm in diameter, 120mm in length;
3. 30s fast alignment, azimuth accuracy 1°; 90s accurate alignment, azimuth accuracy 0.5°;
ER-AHRS-7
1.High performance MEMS gyroscope with gyroscope bias instability <3°/h.
2.Built-in ultra-low-power, high-performance three-axis digital magnetic sensor with a dynamic field range of ±50 gauss.
3.A new generation of high-resolution altimeter sensors including a high linear pressure sensor and an ultra-low power 24-bit ADC with a height resolution of 10 cm.
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.
ER-MIMU-041
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Can find north independently.
ER-MIMU-042
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): 0.03deg/hr.
ER-MIMU-043
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): <0.1deg/hr.
ER-MIMU-044
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. -40~80°C temperature compensation.
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-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.