Inertial Measurement Unit (IMU) PCBA is the core component of inertial navigation systems, integrating three gyroscopes and three accelerometers to measure the aircraft’s angular velocity and linear acceleration. It provides raw sensor data for calculating attitude, position, and velocity, supporting stable flight control and navigation. The PCBA is designed for high precision, fast response, low noise, and low drift, ensuring accurate data collection even in extreme flight conditions (high vibration, extreme temperature). Using industrial-grade components and strict calibration processes, our 200+ professional employees and 7 SMT production lines ensure mass production, with each unit undergoing comprehensive performance testing.