Phone: +86-13992884879

Email: info@ericcointernational.com

Aerospace

Ericco's equipment is widely deployed in aerospace, providing critical support for navigation, stabilization, and control. INS and IMUs deliver precise positioning and orientation data, crucial for aircraft, spacecraft, and missiles, especially when GPS is unavailable. Gyroscopes and accelerometers ensure stability and smooth flight, while attitude and heading reference systems (AHRS) and north seekers offer accurate orientation and heading information. These devices enhance guidance systems, fault detection, and reliability, making them indispensable for high-altitude flights, space exploration, and aerospace research and development.

Ultra Size Oem Stable Control Mems Imu

Ultra-small Size OEM Navigation 2 axis MEMS Gyro

ER-2MG-042
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): 0.03deg/hr.

Ultra Size Oem Navigation Mems Imu

Ultra-small size OEM Navigation MEMS IMU

ER-MIMU-042
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): 0.03deg/hr.

Mapping Level Ultra Precision Gnss Mems Ins

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.

High Precision Mems Integrated Navigation System

High-precision 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.

High Performance Navigation Mems Imu.jpg

High Performance Navigation 2 axis MEMS Gyro

ER-2MG-052
1. OEM;
2. Bias Instability: 0.03º/h;
3. Light Weight.

North Seeking Mems Imu.jpg

Low-cost Attitude-control 2 axis MEMS Gyro

ER-2MG-054
1. OEM;
2. Bias Instability (1σ 25℃): 1º/h;
3. Small Volume.

High Precision Navigation Mems Imu

High Performance 2-Axis MEMS Gyro

ER-2MG-062
1. Smallest Size;
2. Bias Instability(1σ 25℃): 0.03º/h;
3. Light Weight.

Low Power Inertial Measurement Unit

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 Performance Navigation 2 Axis Mems Gyro

High Performance Navigation 2 axis MEMS Gyro

ER-2MG-102
1. Thin;
2. Light weight;
3. Simple structure and good reliability.

Cost Efficient Gnss Aided Mems Ins

Cost-efficient GNSS aided MEMS INS

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 Ins

Low Cost Single Antenna MEMS INS

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 Performance Navigation Mems Imu.jpg

High Performance Navigation MEMS IMU

ER-MIMU-052
1. Size: 70*65*45(with shell)/43.2*43.2*35.5 (without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): 0.03deg/hr.

North Seeking Mems Imu.jpg

Low-Cost Attitude-Control MEMS IMU

ER-MIMU-054
1. Size:70*65*45(with shell)/43.2*43.2*35.5 (without shell and baseboard);
2. -40~80°C temperature compensation;
3. OEM modular design, strong applicability.

High Accuracy North Seeking Mems Imu

High Precision Navigation MEMS IMU

ER-MIMU-062
1. Smallest volume: 38.6mm x 44.8mm x25.5mm;
2. Light weight: ≤70g;
3. Temperature compensation: -40℃~ + 80℃.

Low Power Inertial Measurement Unit

Low Power Inertial Measurement Unit

ER-MIMU-092
1. Mini Diameter: 120mm x Φ30mm;
2. Light weight: ≤150g;
3. Temperature compensation: -40℃~ + 80℃.

Ultra Size Oem Navigation Mems Imu

Ultra-small Size Navigation 3 axis MEMS Gyro

ER-3MG-042
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. Gyro bias instability(1σ 25℃): 0.03deg/hr.

High Performance Navigation Mems Imu.jpg

High Performance Navigation MEMS Gyro

ER-3MG-052
1. OEM;
2. Bias Instability: 0.03º/h;
3. Light Weight.

North Seeking Mems Imu.jpg

Low-cost Attitude-control MEMS Gyro

ER-3MG-054
1. OEM;
2. Bias Instability(1σ 25℃): 1º/h;
3. Light Weight.

2 Axis North Seeking Mems Gyro

High-Precision Navigation MEMS IMU

ER-MIMU-102
1. Small size: 47×44×14mm;
2. Light weight: 40g;
3. Gyro bias instability: 0.03º/h (Allan variance).

High Precision Navigation Mems Imu

High Performance 3-Axis MEMS Gyro

ER-3MG-062
1. Smallest Volume;
2. Bias Instability: 0.03º/h;
3. Light Weight.

Low Power Inertial Measurement Unit

High Performance 3-Axis MEMS Gyro

ER-3MG-092
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.03º/h;
3. Size: 120mm x Φ30mm.

High Performance Navigation 2 Axis Mems Gyro

High Performance Navigation 3 axis MEMS Gyro

ER-3MG-102
1. Thin;
2. Light weight;
3. Simple structure and good reliability.

High Precision Navigation MEMS Gyroscope

High Precision Navigation MEMS Gyroscope

ER-MG2-300/400 (0.03°/hr)
1. Up to ±400°/s measurement range;
2. 0.03°/hr bias instability;
3. 0.01-0.025°/√hr angular random walk.

High Performance Quartz Accelerometer

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)

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

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.

High Performance Quartz Accelerometer

Aerospace Quartz Accelerometer

ER-QA-01A:
1.Bias repeatability: 10μg;
2.Scale factor repeatability: 10ppm;
3. Class II non-linearity repeatability: 10μg/g².

Economical MEMS Gyroscope

Economical MEMS Gyroscope

ER-MG-056 (3°/h)
1. 3°/hr bias instability;
2. 0.25°/√hr angular random walk;
3. 5°/hr bias stability.

High Precision Navigation MEMS Gyroscope

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.

Wide Range Quartz Accelerometer (±70g)

High Accuracy Quartz Accelerometer

ER-QA-01B:
1. Bias repeatability: 30μg;
2. Scale factor repeatability: 30ppm;
3. Widely applied in aerospace.

High Performance Quartz Accelerometer

High-Precision and Anti-Vibration Quartz Accelerometer for Aerospace

ER-QA-02A:
1. Bias repeatability: 60μg;
2. Scale factor repeatability: 60ppm;
3. Class II non-linearity repeatability: 50μg/g².

High Accuracy Mems Accelerometer (2)

High Accuracy MEMS Accelerometer

ER-MA-5 (Alternative of MS1000):
1. Bias instability (Allan Curve) 5 μg;
2. Bias stability (1s Standard Deviation)(1σ)<20μg;
3. Bias month repeatability 100μg.

High Accuracy Mems Accelerometer (3)

Ultra High Precision MEMS Accelerometer

ER-MA-6
1. Large range, ultra-high precision, high reliability and low power consumption;
2. Class II Non-linearity: <10µg/g²;
3. Bias Stability (10s smooth): <5ug;
4. Bias instability (Allan Curve): <2ug.

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