High Performance 3-Axis MEMS Gyro
ER-3MG-062
1. Smallest Volume;
2. Bias Instability: 0.03º/h;
3. Light Weight.
High Precision Stable-control MEMS Gyro
ER-3MG-063
1. Bias Instability (1σ 25℃): 0.3-0.1º/h;
2. Smallest Size;
3. Light Weight.
Low Cost 3-Axis MEMS Gyro
ER-3MG-064
1. Smallest Size;
2. Bias Instability(1σ 25℃): 1º/h;
3. Light Weight.
High Accuracy 3-Axis MEMS Gyro
ER-3MG-091
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.01-0.02º/h;
3. Size: 120mm x Φ30mm.
High Performance 3-Axis MEMS Gyro
ER-3MG-092
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.03º/h;
3. Size: 120mm x Φ30mm.
North Seeking MEMS Inertial Measurement Unit
ER-MIMU-181
1.Gyro bias instability:<0.01 deg/hr;
2.Size:65*51*35.5;
3.Low cost.
High-performance Navigation MEMS IMU
ER-MIMU-182
1.Gyroscope bias instability: 0.03 deg/hr
2.High-performance navigation
3.Weight: 140g.
High-precision Stable-Controlled MEMS IMU
ER-MIMU-183
1.Gyroscope bias instability:<0.1deg/hr;
2.Weight: 140g;
3.-40~80°C temperature compensation.
Low-cost MEMS IMU for Attitude Control
ER-MIMU-184
1.Gyroscopic bias instability: 1 deg/hr.
2. -40~80°C temperature compensation.
3.Low cost.
High Performance MEMS IMU
ER-MIMU-M02
1. Small size: 47×44×14mm;
2. High reliability and strong environmental adaptability.
3. Light weight: 50g.
High Precision Stable-control MEMS Gyro
ER-3MG-093
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.3-0.1º/h;
3. Light Weight.
Low Cost 3-Axis MEMS Gyro
ER-3MG-094
1. Cylinder;
2. Bias Instability (1σ 25℃): 1º/h;
3. Light Weight.
3-Axis North-Seeking MEMS Gyro
ER-3MG-101
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
High Performance Navigation 3 axis MEMS Gyro
ER-3MG-102
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
High Precision Navigation/Stable Control 3 axis MEMS Gyro
ER-3MG-103
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
Low-cost Attitude-control 3 axis MEMS Gyro
ER-3MG-104
1. Thin;
2. Light weight;
3. Simple structure and good reliability.
High Performance MEMS IMU
ER-MIMU-M01A(≤2°/h)
1. Miniaturized IMU;
2. Gyro bias instability: ≤2°/h(Allan variance);
3. High cost performance.
Low Cost 2D Electronic Compass (Single Board)
ER-EC-220:
1. Heading accuracy 1°, tilt range ±5°;
2. Measurement range 0~360°;
3. With hard magnetic, soft magnetic and tilt compensation.
High Performance Quartz Accelerometer
ER-QA-03A:
1. Bias repeatability: 10-50μg;
2. Scale factor repeatability: 15-50ppm;
3. Class II non-linearity repeatability: 10-30μg/g².
Wide Range Quartz Accelerometer (±70g)
ER-QA-03B:
1. Bias repeatability: 10-30μg;
2. Scale factor repeatability: 15-50ppm;
3. Class II non-linearity repeatability: 10-30μg/g².
Small Size Quartz Accelerometer For Aerospace
ER-QA-03C:
1. Bias repeatability: 15-80μg;
2. Scale factor repeatability: 15-80ppm;
3. Class II non-linearity repeatability: 20-50μg/g².
Anti-shock and High-Temp Quartz Accelerometer
ER-QA-03D:
1. High temperature resistance and shock resistance;
2. Excellent repeatability and high reliability;
3. It can be used for both static and dynamic testing.
Ultra-thin Quartz Accelerometer
ER-QA-03E:
1. Bias repeatability: 30-80μg;
2. Scale factor repeatability: 50-100ppm;
3. Class II non-linearity repeatability: 20-30μg/g².
Small Size and High Temperature Quartz Accelerometer (Φ18.2)
ER-QA-03F:
1. Bias repeatability: 150-220μg;
2. Scale factor repeatability: 150-220ppm;
3. Class II non-linearity repeatability: ±40~±50μg/g².