The invention provides an aircraft multi-control-surface coordination control management system which comprises an instruction preliminary distribution module, a reconstruction instruction production module, a control efficiency conversion module, a polarity module, a priority judgment and control surface deviation limiting module and an instruction redistribution module. According to the aircraft multi-control-surface coordinated control management system and method provided by the invention, the functions of coordinated scheduling, instruction conversion, fault reconstruction, deviation limiting protection and the like of multiple groups of functional redundancy control surfaces in different flight stages can be realized, the aerodynamic redundancy of the aircraft is comprehensively played, the flight safety is guaranteed, and the system and the method are compatible with a traditional control law design method, high in applicability and universality and high in practicability. And the engineering value is high.

    本申请提供了一种飞机多操纵面协调控制管理系统,包括:指令初步分配模块、重构指令生产模块、操纵效率转换模块、极性模块、优先级判定及操纵面限偏模块、指令再分配模块,本申请提供的飞机多操纵面协调控制管理系统和方法可以实现多组功能冗余操纵面在不同飞行阶段的协调调度、指令转换、故障重构、限偏保护等功能,全面发挥飞机的气动冗余,保障飞行安全,同传统控制律设计方法兼容,适用性、通用性强,工程价值较高。


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    Titel :

    Coordinated control management system for multiple control surfaces of airplane


    Weitere Titelangaben:

    一种飞机多操纵面协调控制管理系统


    Beteiligte:
    LIU SHIMIN (Autor:in) / ZHENG HUA (Autor:in) / HE CHAO (Autor:in)

    Erscheinungsdatum :

    2022-07-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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