The present invention relates to a flight control computer capable of fault diagnosis through an analytical channel. More particularly, the present invention relates to a flight control computer capable of diagnosing malfunctions through an analytical channel that detects malfunctions and failures of a single or redundant electronic control system applied to an unmanned aerial vehicle or a manned aircraft.

    본 발명은 해석적 채널을 통해 고장진단이 가능한 비행조종 컴퓨터에 관한 것으로서, 더욱 상세하게는, 무인기 또는 유인항공기에 적용된 단일 또는 이중화 전자식 조종시스템의 오작동 및 고장을 검출하는 해석적 채널을 통해 고장진단이 가능한 비행조종 컴퓨터에 관한 것이다.


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    Titel :

    Fault tolerant flight control computer using additional analytical channel


    Weitere Titelangaben:

    해석적 채널을 통해 고장진단이 가능한 비행조종 컴퓨터


    Beteiligte:
    KWANG HYUN LEE (Autor:in)

    Erscheinungsdatum :

    2022-11-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen




    Fault tolerant digital flight control using analytical redundancy

    Poyneer, R.D. / Cunningham, T.B. | Tema Archiv | 1977


    Fault-Tolerant Flight Computer

    Online Contents | 1996


    Fault-Tolerant Flight Computer

    Chau, Savio | NTRS | 1996


    Fault Tolerant Flight Control

    Meir Pachter / Yih-Shiun Huang | AIAA | 2003