ERICCO INERTIAL TECHNOLOGY ER-MIMU-052 High Performance Navigation MEMS IMU Introduction Inertial Measurement Unit (IMU) is a device that measures an object's three-axis attitude angle (or angular velocity) and acceleration. Gyroscopes and accelerometers are the core devices of an Inertial Navigation System (INS). Through the built-in accelerometers and gyroscopes, the IMU can measure the three-axis linear acceleration and three-axis rotational angular velocity, and obtain the attitude, velocity, and displacement information of the carrier through analysis. ER-MIMU-052 uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication. Default baud rate 921600 (customized). 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. A simple operation is required to connect our products to your system and obtain IMU data without the 15-pin plug provided by our company. At the same time, the size and weight of our products can be significantly reduced by removing the base plate housing. Features Size:70*65*45(with shell)/43.2*43.2*35.5 (without shell and baseboard) Weight:220(with shell) /100(without shell and baseboard) OEM, modular design, strong applicability -40~80°C temperature compensation Gyro bias instability: 0.03deg/hr Gyro bias stability (10s 1σ): <0.15deg/hr Gyro angular random walk: <0.01 °/√h Accelerometer bias repeatability: 100ug Accelerometer class II non-linearity coefficient: <100ug/g² High-performance navigation Application Integrated Navigation Systems & Inertial Guidance System Flight Control System Attitude Heading Reference Systems (AHRS) Stabilization of Antennas, Cameras & Platforms Aerial and Marine Geo-mapping / Surveying Whatsapp/Wechat/Mob:8613992884879 Websit : www.ericcointernational.com E-mail : ericco001@ericcointernational.

ERICCO INERTIAL TECHNOLOGY Specifications Item Whatsapp/Wechat/Mob:8613992884879 Websit: www.ericcointernational.com E-mail: [email protected]

ERICCO INERTIAL TECHNOLOGY Product composition and working principle The product is mainly composed of three-axis MEMS accelerometer and gyroscope. The working principle is as follows: the gyroscope and accelerometer data are collected by ARM microcontroller, three high-precision gyroscopes are collected by 1-channel digital interface SPI, and three accelerometers are collected by another 1-channel digital interface SPI. All sensors are calibrated and compensated in software after acquisition. Product technical characteristics A)The product is designed for miniaturization and low power consumption;...

ERICCO INERTIAL TECHNOLOGY Table 1 Pin definition of MIMU high precision inertial measurement unit Whatsapp/Wechat/Mob:8613992884879 Websit: www.ericcointernational.com E-mail: [email protected]

ERICCO INERTIAL TECHNOLOGY The user installs the test interface on the computer, open xInsConnect.exe, as shown below. Click "COMCFG" to configure the baud rate of RS422 serial port, which is the COM port required; Click the "Open" button to open the RS422 communication interface and power on the IMU. The Angle data of X,Y,Z gyro "GX,GY,GZ", the data of X,Y,Z accelerometer "ACCX,ACCY,ACCZ" will be displayed on the interface. The temperature data of IMU will be displayed in the "TX" box. Click "CAL" box to set the data update rate of the interface to 100. The "Counter" box displays the frame serial...

ERICCO INERTIAL TECHNOLOGY CQMCFG Open Close 1) Installation error description Internal orthogonal compensation has been carried out for the whole product. If the platform used by the product cannot guarantee the accuracy of the benchmark after installation, please compensate the installation error accordingly. When the product is installed, it should be tightly installed parallel to the base level of the carrier installation (the installation error with the base level should be less than 0.05°). Because the product is a precision test instrument, although there is a shell protection, in order...