Cost Effective Attitude Control MEMS IMU
ER-MIMU-16(M02A)
1. Small size: 47×44×14mm;
2. Light weight: 40g;
3. Gyro bias instability: 0.3 º/h (Allen variance).
Low cost Inertial Measurement Unit
ER-MIMU-17
1. Small size: 47×44×14mm;
2. Light weight: 40g;
3. Gyro bias instability: 1º/h (Allen variance).
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 Performance North Seeking MEMS Gyroscope
ER-MG2-50/100 (0.01-0.02°/hr)
1. 0.01-0.02°/hr bias instability;
2. 0.0025-0.005°/√hr angular random walk;
3. Small size: 11x11x2mm.
High Precision Navigation MEMS Gyroscope
ER-MG2-300/400 (0.03-0.05°/hr)
1. Up to ±400°/s measurement range;
2. 0.03-0.05°/hr bias instability;
3. 0.01-0.025°/√hr angular random walk.
Economical MEMS Gyroscope
ER-MG-056 (1°/h)
1. 1°/hr bias instability;
2. 0.25°/√hr angular random walk;
3. 5°/hr bias stability.
High Performance MEMS Gyroscope
ER-MG-067 (<0.3°/hr)
1. <0.3°/hr bias instability;
2. <0.125°/√hr angular random walk;
3. 3°/hr bias stability.
High Performance Navigation Grade MEMS Gyroscope
ER-MG2-200 (<0.02°/hr)
1.Up to 200°/s measurement range;
2.<0.02°/hr bias instability;
3.<0.005°/√hr angular random walk.
High Accuracy Single-Axis MEMS Gyro
ER-MG-057 (1°/h)
1. 1°/hr bias instability;
2. 0.2°/√hr angular random walk;
3. 4°/hr bias stability.
High Precision MEMS Gyroscope
ER-MG-068 (<0.3°/h)
1. <0.3°/hr bias instability;
2. <0.125°/√hr angular random walk;
3. Small size: 11 x 11 x 2mm.
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.
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 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.
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 Gyroscope
ER-FOG-910 (0.02º/h)
1. Bias stability: 0.02º/h;
2. Small size: Φ82×26;
3. Long life and high reliability.
GNSS High Precision Positioning Module
ER-GNSS-M01
1. Integrated 9-axis IMU to support onboard integrated navigation;
2. Support L-band, can receive "China precision" to achieve single centimeter level positioning;
3. Support external high performance inertial navigation, improve the precision of integrated navigation.
High Accuracy MEMS Accelerometer
ER-MA-5 (Alternative of MS1000):
1. Bias instability (Allen Curve) 5 μg;
2. Bias stability (1s Standard Deviation)(1σ)<20μg;
3. Bias month repeatability 100μg.
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.
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°.
High Precision Integrated Navigation Positioning Module
ER-GNSS-M02
1. Equipped with a high-precision RTK algorithm engine;
2. Easy to achieve centimeter-level positioning;
3. Small size, low power consumption, easy system integration.
Single-axis Closed-loop Fiber Optic Gyroscope
ER-FOG-36 (≤0.001º/s)
1. Bias stability:≤0.001º/s;
2. Dynamic range: -300~+300º/s;
3. Small size: Φ36×83.6.