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.
Ultra-Small Fiber Optic Integrated Navigation System
ER-FINS-50:
1. Support BDS/GPS/GLONASS/QZSS;
2. Built-in high-performance fiber optic IMU;
3. High level of protection and security level IP67.
Low Cost FOG Gyroscope
ER-FOG-910 (0.02º/h)
1. Bias stability: 0.02º/h;
2. Small size: Φ82×26;
3. Long life and high reliability.
IMU/VRU/AHRS
ER-AHRS-10 (6 deg/hr)
1.Industrial-grade inertial sensors
2.3 ° dynamic attitude accuracy
3.Stable heading output
4.Factory calibrated in full temperaturerange
Low Cost FOG Rate Gyroscope
ER-FOG-25 (≤0.004º/s)
1. Bias stability: ≤0.004º/s;
2. Small size;
3. Dynamic range: -600~+600°/s.
Aerospace Quartz Accelerometer
ER-QA-01A:
1.Bias repeatability: 10μg;
2.Scale factor repeatability: 10ppm;
3. Class II non-linearity repeatability: 10μg/g².
Low Cost Wireless Tilt Sensor
ER-TS-4296 Features:
1. Biaxial tilt monitoring;
2. Input voltage DC 9~36V;
3. Full range accuracy 0.1°, resolution 0.01°.
Small Size FOG Gyroscope
ER-FOG-50 (0.2~2.0º/h)
1. Bias stability: 0.2~2.0º/h;
2. Small size: Φ50mm×38mm;
3. Digital closed loop mode.
Digital Wireless Transmission Dual-axis Tilt Sensor
ER-TS-5296 Features:
1. Accuracy: 0.1°, resolution: 0.01°;
2. Dual-axis inclination monitoring (single-axis optional);
3. Frequency response: 100HZ.
Industrial Grade Wireless Tilt Sensor
ER-TS-5297 Features:
1. Accuracy: 0.1°, resolution: 0.01°;
2. High vibration resistance>3500g;
3. Measurement Range: ±0~±90°(optional).
High Precision Wireless Transmission Tilt Sensor
ER-TS-12200-Modbus Features:
1. Dual axis monitoring (single axis optional);
2. Full range accuracy 0.001°, resolution 0.0005°;
3. Volume (94*74*64mm) (customizable).
Standard Precision GNSS Navigation and Positioning Module
ER-GNSS-M04
1.Universal size GNSS module, hardware compatible with previous products, mainstream GPS module, easy to replace;
2. Excellent navigation and positioning performance, supporting single system independent;
3. Positioning and multi-system joint positioning.