Phone: +86-13992884879

Email: info@ericcointernational.com

Land Vehicle

Inertial devices are crucial for land vehicles, providing precise navigation, stabilization, and control. INS and IMUs offer accurate positioning even when GPS signals are weak or unavailable. Gyroscopes and accelerometers enhance vehicle stability and control, essential for smooth driving and advanced safety systems. These devices support autonomous and advanced driver-assistance systems (ADAS) by providing real-time motion data. They also aid in dead reckoning, vehicle dynamics monitoring, and mapping applications. Overall, inertial devices ensure optimal performance, safety, and reliability for land vehicles across various applications.

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.

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 Precision FOG North Seeker

High Precision FOG North Seeker

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.

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.

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 Precision Stable Controlled Mems Inertial Measurement Unit

High-precision Stable-Controlled MEMS IMU

ER-MIMU-183
1.Gyroscope bias instability:<0.1deg/hr;
2.Weight: 140g;
3.-40~80°C temperature compensation.

Low Cost Mems Inertial Measurement Unit For Attitude Control

Low-cost MEMS IMU for Attitude Control

ER-MIMU-184
1.Gyroscopic bias instability: 1 deg/hr.
2. -40~80°C temperature compensation.
3.Low cost.

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