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.

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.

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 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

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°.

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 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℃.

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).

Stable Control Mems Imu

High Precision Stable-control MEMS Gyro

ER-3MG-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 3-Axis MEMS Gyro

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

High Performance Mems Imu

High Performance MEMS IMU

ER-MIMU-M02
1. Small size: 47×44×14mm;
2. High reliability and strong environmental adaptability.
3. Light weight: 50g.

Miniaturized Mems Imu

High Precision Stable-control MEMS Gyro

ER-3MG-093
1. Cylinder;
2. Bias Instability (1σ 25℃): 0.3-0.1º/h;
3. Light Weight.

Small Size Mems Imu

Low Cost 3-Axis MEMS Gyro

ER-3MG-094
1. Cylinder;
2. Bias Instability (1σ 25℃): 1º/h;
3. Light Weight.

High Precision Navigation Stable Control 2 Axis Mems Gyro

High Precision Navigation/Stable Control 3 axis MEMS Gyro

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

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