Phone: +86-13992884879

Email: info@ericcointernational.com

UAV

In today's era of rapid development of UAV technology, Inertial Measurement Unit (IMU) plays a key role as one of the most important sensors in UAV navigation systems. ERICCO's self-developed MEMS IMU can measure the acceleration and angular velocity of the aircraft in space in real time, providing accurate attitude, position and velocity information for drones. Gyroscope and accelerometer in IMU. The built-in gyroscope is used to measure the angular rate of rotation of the body around its own axis, that is, the rotation speed of the object. The accelerometer is used to measure the linear velocity. Therefore, it is of great significance to deeply study the application of IMU in drone navigation and related issues.

Ultra Size Oem Navigation Mems Imu

Ultra-small Size OEM Navigation-Stable Control 2 axis MEMS Gyro

ER-2MG-043
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℃): <0.1deg/hr.

Ultra Small Size Oem Attitude Control Mems Imu

Ultra small Size OEM Attitude Control 2 axis MEMS Gyro

ER-2MG-044
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. -45~85°C temperature compensation.

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.

High Performance Dynamic FOG North Seeker

High Performance Dynamic FOG North Seeker

ER-FNS-01 (0.02°-0.5°):
1. With internal shock absorbers, it can adapt to large shocks and vibrations;
2. Quick alignment in 30 seconds, precise alignment in 90 seconds;
3. Not affected by magnetic fields.

Ultra Size Oem Stable Control Mems Imu

Ultra-Small size OEM Stable Control MEMS IMU

ER-MIMU-043
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℃): <0.1deg/hr.

Ultra Small Size Oem Attitude Control Mems Imu

Ultra-small size OEM Attitude-control MEMS IMU

ER-MIMU-044
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. -40~80°C temperature compensation.

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 Precision Stable Control Mems Imu.jpg

High Precision Navigation/Stable Control 2 axis MEMS Gyro

ER-2MG-053
1. OEM;
2. Bias Instability (1σ 25℃): 0.3-0.1º/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.

Stable Control Mems Imu

High Precision Stable-control 2 axis MEMS Gyro

ER-2MG-063
1. Bias Instability(1σ 25℃): 0.3-0.1º/h;
2. Smallest Size;
3. Light Weight.

Low Cost Mems Inertial Measurement Unit

Low Cost 2-Axis MEMS Gyro

ER-2MG-064
1. Smallest Size;
2. Bias Instability (1σ 25℃): 1º/h;
3. Light Weight.

Miniaturized Mems Imu

High Precision Stable-control 2 axis MEMS Gyro

ER-2MG-093
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.3-0.1º/h;
3. Size: 120mm x Φ30mm.

Small Size Mems Imu

Low Cost 2-Axis MEMS Gyro

ER-2MG-094
1. Cylinder;
2. Bias Instability (1σ 25℃): 1º/h;
3. Size: 120mm x Φ30mm.

High Precision Navigation Stable Control 2 Axis Mems Gyro

High Precision Navigation/Stable Control 2 axis MEMS Gyro

ER-2MG-103
1. Thin;
2. Light weight;
3. Simple structure and good reliability.

Low Cost Attitude Control 2 Axis Mems Gyro

Low-cost Attitude-control 2 axis MEMS Gyro

ER-2MG-104
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.

High Performance Dynamic Fog North Seeker

High-performance Dynamic FOG North Seeker

ER-FNS-01D
1.Internal shock absorber, can adapt to large impact and vibration;
2.30s fast alignment, azimuth accuracy 1°; 90s accurate alignment, azimuth accuracy 0.5°;
3.Dynamic north finding, accurate north finding and attitude following in the case of vibration;

Low Cost 3 Axis Fog North Seeker

Low Cost 3 Axis FOG North Seeker

ER-FNS-03 (0.5°-1°):
1. Low cost FOG north seeking solution;
2. Specially suitable for mining application;
3. 3-axis FOG & 3-axis accelerometer.

High Accuracy North Seeking Mems Imu

Smallest Volume MEMS North Seeker

ER-MNS-06 (0.25°-1°):
1. Smallest Volume MEMS north seeker in the world;
2. Resistant to harsh environment;
3. Light weight, low power consumption.

High Performance Navigation 2 Axis Mems Gyro

The Thinnest and Lightest MEMS North Seeker

ER-MNS-10 (0.25°-1°):
1. The thinnest and lightest MEMS north seeker (40g);
2. High-precision MEMS gyroscopes and accelerometers;
3. High stability and reliability.

High Precision Stable Control Mems Imu.jpg

High Precision Stable Control MEMS IMU

ER-MIMU-053(Previous ER-MIMU-03)
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℃): <0.1deg/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.

Stable Control Mems Imu

Stable-Control MEMS IMU

ER-MIMU-063(Previous ER-MIMU-07)
1. Smallest volume: 38.6mm x 44.8mm x25.5mm;
2. Light weight: ≤70g;
3. Temperature compensation: -40℃~ + 80℃.

Low Cost Mems Inertial Measurement Unit 2

Low Cost MEMS Inertial Measurement Unit

ER-MIMU-064
1. Smallest volume: 38.6mm x 44.8mm x25.5mm;
2. Light weight: ≤70g;
3. Temperature compensation: -40℃~ + 80℃.

Miniaturized Mems Imu

Miniaturized MEMS IMU

ER-MIMU-093
1. Mini diameter: 120mm x Φ30mm;
2. Light weight: ≤150g;
3. Temperature compensation: -40℃~ + 80℃.

Small Size Mems Imu

Small Size MEMS IMU

ER-MIMU-094
1. Mini diameter: 120mm x Φ30mm;
2. Light weight: ≤150g;
3. Temperature compensation: -40℃~ + 80℃.

High Precision Stable Controlled Mems Inertial Measurement Unit

High-precision Stable-Controlled 2 axis MEMS Gyro

ER-2MG-183
1.Gyro bias instability: < 0.3 deg/hr;
2.Gyro bias stability (10s 1σ): < 1 deg/hr;
3.Gyro angle random walk: < 0.05 °/√h.

Low Cost Mems Inertial Measurement Unit For Attitude Control

Low-cost 2 axis MEMS Gyro

ER-2MG-184
1.Weight: 140;
2.Gyro bias instability: 1 deg/hr;
3.Gyro bias stability (10s 1σ): 4 deg/hr.

North Seeking Mems Inertial Measurement Unit

High Reliability MEMS North Seeker

ER-MNS-18
1.High performance heading accuracy up to 0.25°secψ(1σ);
2.Low power consumption and wide voltage;
3.Resistant to harsh environment.

Ultra Size Oem Stable Control Mems Imu

Ultra-small Size Navigation/Stable Control MEMS Gyro

ER-3MG-043
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℃): <0.1deg/hr.

Ultra Small Size Oem Attitude Control Mems Imu

Ultra-Small Size Attitude-control 3-axis MEMS Gyro

ER-3MG-044
1. Size: 40*40*42(with shell)/27*26*34(without shell and baseboard);
2. OEM, modular design, strong applicability;
3. -40~80°C temperature compensation.

High Precision Stable Control Mems Imu.jpg

Navigation/Stable Control MEMS Gyro

ER-3MG-053
1. OEM;
2. Bias Instability(1σ 25℃): 0.3-0.1º/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.

High Precision Navigation Stable Control 2 Axis Mems Gyro

Stable Control MEMS IMU

ER-MIMU-103(Previous ER-MIMU-16)
1. Small size: 47×44×14mm;
2. Light weight: 40g;
3. Gyro bias instability: 0.1 º/h (Allan variance).

High Performance Navigation 2 Axis Mems Gyro

Low-cost Attitude Control MEMS IMU

ER-MIMU-104(Previous ER-MIMU-17)
1. Small size: 47×44×14mm;
2. Light weight: 40g;
3. Gyro bias instability: 1º/h (Allan variance).

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