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.

North Seeking Mems Imu For Gyro Tools 3 (1)

MEMS Gyro Directional Module for GWD

ER-Gyro-15
1.Adopt the latest three-axis MEMS gyro, three-axis MEMS plus meter strapdown inertial measurement technology;
2.Subvert the size of traditional gyro tools, extremely small, with a diameter of only 30mm and a length of 120mm, which can be easily embedded in the narrow front-end space such as the probe tube;
3.All-solid-state design, excellent impact and vibration resistance;

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.

High Cost Performance Ahrs

High Cost Performance AHRS

ER-AHRS-7
1.High performance MEMS gyroscope with gyroscope bias instability <3°/h.
2.Built-in ultra-low-power, high-performance three-axis digital magnetic sensor with a dynamic field range of ±50 gauss.
3.A new generation of high-resolution altimeter sensors including a high linear pressure sensor and an ultra-low power 24-bit ADC with a height resolution of 10 cm.

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.

High Precision Mems Integrated Navigation System

Cost-effective 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.

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

Low-cost MEMS Integrated Navigation System

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.

MEMS Gyro Directional Module for MEMS Directional Drilling/Drilling Directional Instrument

ER-MNS-09(0.25°-1°):
1.Adopt the latest MEMS gyro technology, cylindrical design, its diameter is reduced to 30mm, length is 120mm, can be easily embedded in the narrow space at the front of the drilling equipment (such as the probe);
2.Adopt the latest three-axis MEMS gyro, three-axis MEMS plus meter strapdown inertial measurement technology;
3.Full solid-state design, built-in inner platform, excellent impact and vibration resistance, and resistant to harsh environments.

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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.

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℃.

High Performance Navigation Mems Inertial Measurement Unit

High-performance Navigation 2 axis MEMS Gyro

ER-2MG-182
1.Gyro bias instability: 0.03 deg/hr;
2.Gyro bias stability (10s 1σ): <0.15deg/hr;
3.Gyro angle random walk: <0.025 °/√h.

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.

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 Mems Inertial Measurement Unit

High-performance Navigation MEMS IMU

ER-MIMU-182
1.Gyroscope bias instability: 0.03 deg/hr
2.High-performance navigation
3.Weight: 140g.

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 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.

High Performance Navigation Mems Inertial Measurement Unit

High-performance Navigation 3 axis MEMS Gyro

ER-3MG-182
1.Gyro bias instability: 0.03 deg/hr;
2.Gyro bias stability (10s 1σ): <0.15 deg/hr;
3.Gyro angle random walk: <0.01°/√h.

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.

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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