본 발명은 무인항공기의 작동기 신호처리모듈에 관한 것으로서, 더욱 구체적으로는 작동기 신호처리모듈을 이용하여 무인항공기의 로터 주변 작동기 및 센서들을 모니터링하고 제어하는 방법에 관한 것이다. 구체적으로 복수의 나셀을 포함하는 틸트로터 항공기는 통합 비행제어장치(IFCC, Integrated Flight Control Computer). 복수의 나셀 각각에 포함된 전자변속기(ESC, Electronic Speed Controller), 복수의 나셀 각각에 포함된 적어도 하나의 센서 및 복수의 나셀 각각에 포함된 작동기 신호처리장치(ASPM, Actuator Signal Processing Module)를 포함하고, 작동기 신호처리장치는 적어도 하나의 센서에서 감지된 결과를 통합 비행제어장치로 송신하고, 통합 비행제어장치로부터 전자변속기를 제어하기 위한 명령을 수신하면 명령에 대응하는 신호를 전자변속기로 전달한다.

    The present invention relates to an actuator signal processing module of an unmanned aerial vehicle and, more specifically, to a method for monitoring and controlling an actuator and sensors around a rotor of an unmanned aerial vehicle by using an actuator signal processing module. To this end, a tilt-rotor aerial vehicle including a plurality of nacelles comprises: an integrated flight control computer (IFCC); an electronic speed controller (ESC) included in each of the plurality of nacelles; at least one sensor included in each of the plurality of nacelles; and an actuator signal processing module (ASPM) included in each of the plurality of nacelles. Here, the actuator signal processing module transmits the result detected by the at least one sensor to the integrated flight control computer, and, after receiving a command for controlling the electronic speed controller from the integrated flight control computer, delivers a signal corresponding to the command to the electronic speed controller. Therefore, the weight of the unmanned aerial vehicle can be reduced.


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    Titel :

    ACTUATOR SIGNAL PROCESSING MODULE AND THE CONTROLLING METHOD THEREOF


    Weitere Titelangaben:

    작동기 신호처리모듈 및 이의 제어방법


    Erscheinungsdatum :

    2020-07-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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