A Navigation System For Integrating Star Sensor and Gyroscope

摘要

The present invention provides a specific sensor and in the integrated navigation system which combines a gyroscope, an inertial sensor and the stars which detects the inertia information of the sensor, air vehicle by detecting the specific image by capturing an image of each image combined with the flight control computer, from a specific detection information detected by the detection unit and calculates the position information of the vehicle, and calculates an angular speed information of the vehicle from the inertial information detected by the inertia sensor, the air vehicle from the position information and angular velocity information from the calculated vehicle calculating the precise position and includes a navigation computer to be transmitted to the flight control computer.