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.
ER-QA-03C:
1. Bias repeatability: 15-80μg;
2. Scale factor repeatability: 15-80ppm;
3. Class II non-linearity repeatability: 20-50μg/g2.
ER-DSPC-10
1. Deep submicron physical design;
2. Unified integrated development environment;
3. Fully autonomous C compiler.
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.
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.
ER-MIMU-06 (0.05º/h) Features:
1. Measuring range ±400º/s;
2. Bias instability (Allan variance) 0.05º/h;
3. Light Weight.
ER-2MG-05 (<0.02º/h)
1. Light Weight;
2. Bias Instability: <0.02;
3. Small Volume.
ER-FOG-910 (0.02º/h)
1. Bias stability: 0.02º/h;
2. Small size: Φ82×26;
3. Long life and high reliability.
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.
ER-FOG-25 (≤0.004º/s)
1. Bias stability: ≤0.004º/s;
2. Small size;
3. Dynamic range: -600~+600°/s.
ER-TS-4296 Features:
1. Biaxial tilt monitoring;
2. Input voltage DC 9~36V;
3. Full range accuracy 0.1°, resolution 0.01°.
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.
ER-FOG-36 (≤0.001º/s)
1. Bias stability:≤0.001º/s;
2. Dynamic range: -300~+300º/s;
3. Small size: Φ36×83.6.
ER-GNSS-M03
1. Suppression technology;
2. Support interference detection and deception detection;
3. Support single star timing.
ER-2MG-06 (0.1º/h)
1. Light Weight;
2. Bias Instability: 0.1º/h;
3. Small Volume.
ER-TS-5296 Features:
1. Accuracy: 0.1°, resolution: 0.01°;
2. Dual-axis inclination monitoring (single-axis optional);
3. Frequency response: 100HZ.
ER-TS-5297 Features:
1. Accuracy: 0.1°, resolution: 0.01°;
2. High vibration resistance>3500g;
3. Measurement Range: ±0~±90°(optional).
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-FNS-02 (0.02°-0.1°):
1. High precision initial alignment & direction control solution;
2. FOG and quartz accelerometer as core sensors;
3. High stability and reliability.
ER-2MG-07 (<0.3º/h)
1. Bias Instability: <0.3º/h;
2. Small Volume;
3. Light Weight.
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).
ER-GNSS-M05
1. Ultra-small package;
2. Compact design and small size;
3. Low power design.
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.
ER-2MG-08 (≤1º/h)
1. Small Volume;
2. Bias Instability: ≤1º/h;
3. Light Weight.
ER-GNSS-M08
1. Support dual-frequency multi-system on-chip RTK positioning solution;
2. RTK update rate up to 10Hz;
3. Supports four systems L1+L2 or L1+L5 working simultaneously.