ERICCO INERTIAL TECHNOLOGY ER-MIMU-182 High-performance Navigation MEMS IMU Introduction The Inertial Measurement Unit (IMU) is a device that measures the three-axis attitude angles (or angular velocities) and accelerations of an object. Gyroscopes and accelerometers are the core components of an Inertial Navigation System (INS). By using the built-in accelerometers and gyroscopes, the IMU can measure the three-axis linear accelerations and three-axis rotational angular velocities, and obtain the information of the carrier's attitude, velocity and displacement through analysis. The ER-MIMU-182 uses high-quality and highly reliable MEMS accelerometers and gyroscopes. Feature Gyroscope bias instability: 0.03 deg/hr Gyroscope bias stability (10s 1σ): <0.5 deg/hr Gyroscope angle random walk: <0.025 °/√h Accelerometer bias repeatability: 100 ug Accelerometer second-order non-linearity: <100 ug/g² High-performance navigation Application Integrated navigation system and inertial guidance system Flight control system Attitude and heading reference system (AHRS) Stability of antennas, cameras and platforms Aeronautical and marine geographic surveying / mapping Whatsapp/Wechat/Mob:8613992884879 Websit : www.ericcointernational.com E-mail : [email protected]

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

ERICCO INERTIAL TECHNOLOGY Wh a tsapp/Wech a t/Mo b:8613992884879 Websit: www.ericcointernational.com E-mail: [email protected]