The invention belongs to the technical field of flight control, and relates to an aircraft longitudinal and transverse control authority distribution method and device based on thrust control. The method comprises the following steps of: S1, distributing all control permissions except a maximum limit value of transverse differential thrust to a longitudinal channel; s2, acquiring a manipulated variable used by a longitudinal channel in real time; and S3, calculating the residual authority of the transverse channel according to the manipulated variable used by the longitudinal channel in real time, and distributing the residual authority to the transverse channel. According to the method, the longitudinal instruction is taken as the priority, the transverse authority is dynamically distributed in real time, and the flight control safety is improved.

    本申请属于飞行控制技术领域,涉及一种基于推力操纵的飞机纵横向控制权限分配方法及装置。该方法包括:步骤S1、将横向差动推力最大限制值以外的所有操纵权限全部分配给纵向通道;步骤S2、获取纵向通道实时使用的操纵量;步骤S3、根据纵向通道实时使用的操纵量计算横向通道的剩余权限,并将剩余权限分配给横向通道。本申请以纵向指令为优先,对横向权限进行实时动态分配,提升了飞行控制安全。


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    Titel :

    Airplane longitudinal and transverse control authority distribution method and device based on thrust control


    Weitere Titelangaben:

    一种基于推力操纵的飞机纵横向控制权限分配方法及装置


    Beteiligte:
    GONG LEI (Autor:in) / ZHANG SHUGUANG (Autor:in) / HE JINGJING (Autor:in)

    Erscheinungsdatum :

    12.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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