An auto-alignment laser pointing system is provided. The auto-alignment laser pointing system is used in an aircraft and includes a light source module, a beam control device, a tracking receiving module, and a gyroscope. The light source module is used for generating laser beam. The beam control device corresponds to the light source module, is disposed in a path of the laser beam, and controls the laser beam to form a projection beam based on a set attitude angle. The tracking receiving module is used for tracking the aircraft and receiving the projection beam, so as to know flight information of the aircraft. The gyroscope is electrically connected to the beam control device to detect an actual attitude angle of the beam control device. When a deviation angle is between the actual attitude angle and the set attitude angle, the beam control device is controlled by the gyroscope to rotate for eliminating the deviation angle, so the projection beam is ensured projecting to the tracking receiving module.


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    Titel :

    AUTO-ALIGNMENT LASER POINTING SYSTEM


    Beteiligte:
    CHUNG HUNG-PIN (Autor:in) / FAN SHIH-JU (Autor:in)

    Erscheinungsdatum :

    20.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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