陀螺仪和加表的输出进行惯导结算

资 源 简 介

利用陀螺仪和加表的输出进行惯导结算，得到飞机的位置，速度，姿态角

详 情 说 明

To obtain the position, velocity, and attitude angles of an aircraft, the outputs from a gyroscope and accelerometer are processed through inertial navigation. This process, known as inertial navigation, utilizes the principles of gyroscopic stabilization to maintain orientation and accelerometer readings to track changes in velocity. Through this method, the aircraft's position and movement can be accurately determined over time, allowing for precise navigation and control.