The invention relates to a rotorcraft, an operation method thereof, and a flight control computer. The rotorcraft comprises a pilot control having a sensor that generates pilot control position data,a flight control that controls a flight characteristic of the rotorcraft, a trim system connected to the pilot control and configured to move the pilot control, and a flight control computer (FCC) configured to receive the pilot control position data from the sensor. The FCC executes a first flight control process and generates, according to the first flight control commands, a trim signal indicating a target position for the pilot control and to send the trim signal to the trim system. The trim system attempts to move the pilot control to the target position to reflect a position of the flight control, and to monitor a working state of the trim system and execute a retrim process in response to determining that the trim system has failed.

    本发明涉及旋翼飞行器及其操作方法、以及飞行控制计算机。旋翼飞行器包括:飞行员控制装置,其具有生成飞行员控制装置位置数据的传感器;飞行控制装置,其控制旋翼飞行器的飞行特性;配平系统,其连接至飞行员控制装置并且被配置成移动飞行员控制装置;以及飞行控制计算机(FCC),其被配置成从传感器接收飞行员控制装置位置数据。FCC执行第一飞行控制过程并且根据第一飞行控制命令生成指示飞行员控制装置的目标位置的配平信号并且将配平信号发送至配平系统以使配平系统尝试将飞行员控制装置移动至目标位置以反映飞行控制装置的位置,并且监测配平系统的工作状态并且响应于确定配平系统已经出现故障而执行重新配平过程。


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    Title :

    Rotorcraft, operation method thereof, and flight control computer


    Additional title:

    旋翼飞行器及其操作方法、以及飞行控制计算机


    Contributors:

    Publication date :

    2020-10-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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