Ultra-small size OEM Attitude-control MEMS IMU
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.
Mapping-level & Ultra-precision GNSS/MEMS INS
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.
Cost-effective MEMS Integrated Navigation System
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.
2-Axis North-Seeking MEMS Gyro
ER-2MG-051
1. OEM;
2. Bias Instability (1σ 25℃): 0.01~0.02º/h;
3. Light Weight.
High Performance Navigation 2 axis MEMS Gyro
ER-2MG-052
1. OEM;
2. Bias Instability: 0.03º/h;
3. Light Weight.
High Precision Navigation/Stable Control 2 axis MEMS Gyro
ER-2MG-053
1. OEM;
2. Bias Instability (1σ 25℃): 0.3-0.1º/h;
3. Light Weight.
Low-cost Attitude-control 2 axis MEMS Gyro
ER-2MG-054
1. OEM;
2. Bias Instability (1σ 25℃): 1º/h;
3. Small Volume.
High Accuracy 2-Axis MEMS Gyro
ER-2MG-061
1. Smallest Size;
2. Bias Instability(1σ 25℃): 0.01-0.02º/h;
3. Light Weight.
High Performance 2-Axis MEMS Gyro
ER-2MG-062
1. Smallest Size;
2. Bias Instability(1σ 25℃): 0.03º/h;
3. Light Weight.
High Precision Stable-control 2 axis MEMS Gyro
ER-2MG-063
1. Bias Instability(1σ 25℃): 0.3-0.1º/h;
2. Smallest Size;
3. Light Weight.
Low Cost 2-Axis MEMS Gyro
ER-2MG-064
1. Smallest Size;
2. Bias Instability (1σ 25℃): 1º/h;
3. Light Weight.
High Accuracy 2-Axis MEMS Gyro
ER-2MG-091
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.01-0.02º/h;
3. Size: 120mm x Φ30mm.
High Performance 2-Axis MEMS Gyro
ER-2MG-092
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.03º/h;
3. Size: 120mm x Φ30mm
High Precision Stable-control 2 axis MEMS Gyro
ER-2MG-093
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.3-0.1º/h;
3. Size: 120mm x Φ30mm.
Low Cost 2-Axis MEMS Gyro
ER-2MG-094
1. Cylinder;
2. Bias Instability (1σ 25℃): 1º/h;
3. Size: 120mm x Φ30mm.
2-Axis North-Seeking MEMS Gyro
ER-2MG-101
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
High Performance Navigation 2 axis MEMS Gyro
ER-2MG-102
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
High Precision Navigation/Stable Control 2 axis MEMS Gyro
ER-2MG-103
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
Low-cost Attitude-control 2 axis MEMS Gyro
ER-2MG-104
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
Low-cost MEMS Integrated Navigation System
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.
Low Cost Single Antenna MEMS Integrated Navigation System
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°.
High Precision Fiber Optic Inertial Navigation System
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.
High Accuracy FOG IMU
ER-FIMU-40:
1.No wearing parts, long service life and high reliability
2. Small in size, light in weight, and easy to integrate
3. Fast dynamic response, suitable for complex motion scenarios
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.