A flight control system (20) for an aircraft and an aircraft include an actuator group (18) and a flight control computer group, the actuator group is used to control the aircraft, the flight controlcomputer group is only composed of a host computer group (10a, 10b, 10c, 10d) of duplex type and at least one backup computer (17). All the host computers are configured to implement the autopilot rules of the aircraft. The host computer group includes: two computers (10a, 10b) of a first hardware type, the computers configured to control the actuators in the actuator group according to a first tolerance level; two computers (10c, 10d) of the first hardware type and second hardware type, the computer being configured to control the actuators in the actuator group according to a second tolerance level, the second tolerance level is not as strict as the first tolerance level.

    一种用于飞行器的飞行控制系统(20)和飞行器包括致动器组(18)和飞行控制计算机组,所述致动器组用于控制所述飞行器,所述飞行控制计算机组仅由双工类型的主计算机组(10a、10b、10c、10d)和至少一个备份计算机(17)构成。所有所述主计算机都被配置成实施所述飞行器的自动驾驶规则。所述主计算机组包括:第一硬件类型的两个计算机(10a,10b),所述计算机被配置成根据第一容差水平控制所述致动器组中的致动器;以及不同于所述第一硬件类型的第二硬件类型的两个计算机(10c,10d),所述计算机被配置成根据第二容差水平控制所述致动器组中的致动器,所述第二容差水平不如所述第一容差水平严格。


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    Title :

    FLIGHT CONTROL SYSTEM FOR AIRCRAFT AND AIRCRAFT


    Additional title:

    用于飞行器的飞行控制系统和飞行器


    Contributors:
    FERVEL MARC (author)

    Publication date :

    2020-06-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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