High Precision NavigationStable Control MEMS IMU

High Precision Navigation/Stable Control MEMS IMU

ER-MIMU-03 (<0.3 deg/hr)
1. 3 axis gyroscope & 3-axis accelerometer;
2. Operate Temp:-40℃~ + 80℃;
3. Gyro bias instability: <0.3 deg/hr.

High Precision Navigation/Stable Control MEMS IMU

High Precision NavigationStable Control MEMS IMU

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Introduction

Introduction of High Precision NavigationStable Control MEMS IMUApplication areas of High Precision NavigationStable Control MEMS IMUHigh-Precision-NavigationStable-Control-MEMS-IMU for Heading

High Precision Navigation/Stable Control MEMS IMU

Introduction
Inertial Measurement Unit, referred to as IMU, is a device to measure the attitude angle (or angular velocity) and acceleration of the three axis of the object. Gyroscope and accelerometer are the core devices of inertial navigation system (INS). With the built-in accelerometer sensor and gyroscope, the IMU can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity and displacement information of the carrier through the resolving.
ER-MIMU-03 uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication, baud rate can be flexibly set between 230400~921600, through the communication protocol to set the user’s required communication baud rate. With X, Y, Z three-axis precision gyro, X, Y, Z three-axis accelerometer with high resolution, can be output by RS422 X, Y, Z three axis of gyroscope and accelerometer’s original hexadecimal complement data (including gyro hexadecimal complement the numerical temperature, angle, the accelerometer hexadecimal temperature, the acceleration hexadecimal complement number); It can also output float dimensionless values of the gyroscope and accelerometer processed by the underlying calculation.

Application 
Azimuth, attitude, position measuring and keeping In GNSS-assisted INS
Heading , pitch ,roll measuring In AHRS for UAV
Motion survey and keeping in MRU
Attitude & azimuth keeping, positioning in IMU
Guidance, navigation, control in tactical MEMS weapon system
Stabilizing & Pointing in satellite antenna,target tracking system
Robotic Control & Orientation in Autonomous machines, Unmanned vehicles

Specifications

ItemParameterUnit
Gyro performance
Range400deg/s
Bandwidth (-3dB)250Hz
Scale Factor at 25°C16000LSB/deg/s
Scale Factor Repeatability (1σ)<50ppm
Scale Factor VS Temperature (1σ)300ppm
Scale Factor Non-Linearity (1σ)<300ppm
Bias Instability<0.3deg/hr
Bias stability (10s 1σ)<3deg/hr
Angular Random Walk<0.15°/ √h
Bias Run-Run (1σ)<1deg/hr
Accelerometer performance
Range1040g
Nonlinearity0.11.3% FSR
Cross Axis Sensitivity11%
Bandwidth2.42.4Hz
Bias Repeatability55mg
Bias Temp Coefficient<0. 5<0. 5mg/°C
Factor Scale Repeatability<0.10.2%
Factor Scale Temp Coefficient±0.01±0.01%/°C
Factor Scale800000200000μg/LSB
System Performance
Supply Voltage6~12V
Supply Consumption2W
InterfaceRS422
Vibration6.06g (10~2000Hz)
Shock5000g, 0.1ms
Operate Temp-40℃~ + 80℃
Storage Temp-55℃~ + 105℃
Weight≤100g (without shell)

≤220g (with shell)

Size43.2mm*43.2mm*35.5mm (without shell)

65mm*70mm*45.5mm (with shell)


Application Techniques

1.IMU working principle & Tactical grade IMU product recommendations

2.How Does an IMU Work?

3.Choosing an IMU: FOG IMUs vs MEMS IMUs

4.Application of IMU in the Field of Drones

5.What is the Difference Between IMU and AHRS?

6.How is IMU used?


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