The invention provides an automatic trim system and method for a turning system of an aircraft. In the normal mode, normal turning operation can be performed. In the automatic trimming mode, the system can automatically identify the taxiing direction and the lateral deviation of the aircraft and automatically correct the taxiing direction and the lateral deviation so that the aircraft can keep linear taxiing. And after the automatic trimming mode is finished, the correction value is written into the turning system, and the zero position of the turning system is finely adjusted, so that lateral deviation can be eliminated when the aircraft slides in the normal mode, the workload of a pilot is reduced, and the safety of the aircraft is improved.

    本发明提供了一种用于飞机的转弯系统的自动配平系统和方法。在正常模式下,能够进行正常的转弯操纵。在自动配平模式下,系统可自动识别飞机的滑行方向和侧偏量,并自动进行修正以使飞机保持直线滑行。在自动配平模式结束后,将修正量写入到转弯系统,对转弯系统的零位进行微调,使得飞机在正常模式下的滑行能够消除侧偏,降低飞行员的工作负担,提升飞机的安全性。


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    Titel :

    Automatic balancing system and method for airplane turning system


    Weitere Titelangaben:

    一种飞机转弯系统自动配平系统和方法


    Beteiligte:
    LIU LEILEI (Autor:in) / WANG HAO (Autor:in) / LIU YALONG (Autor:in) / LI LINWEN (Autor:in)

    Erscheinungsdatum :

    14.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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