The present subject matter relates to an aircraft stabilization system (200). The aircraft stabilization system (200), amongst other components, may include multiple sensors (202), a processing unit (206), and multiple stabilization units (208). The sensors (202) provides sensor data (204). The sensor data (204) is received by the processing unit (206) which may calculate aircraft stabilization parameters based on the sensor data (204). The stabilization units (208) may generate signals based on the aircraft stabilization parameters. The generated signals may be sent to one more stabilization units (208) which may include at least one microcontroller and at least one actuator such as servo motors, hydraulic locks, inflatable rafts, and the like. The actuators, upon receiving the generated signals, operates to counteract tilt caused from maneuvering or vibrations caused due to turbulence.


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    Title :

    AIRCRAFT STABILIZATION SYSTEM


    Additional title:

    FLUGZEUGSTABILISIERUNGSSYSTEM
    SYSTÈME DE STABILISATION D'AÉRONEF


    Contributors:

    Publication date :

    2020-01-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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