飞行器(100)可以包括控制单元(310),被配置为发送控制信号以控制飞行器(100)的飞行;推进单元(110),被配置为控制飞行器的姿态;推进控制器,被配置为基于控制信号将命令发送到推进单元(110)中的对应推进单元;和惯性测量单元(IMU 320)。每个IMU(320)被配置为向推进控制器中的对应的一个推进控制器提供姿态信息。以此方式,对于每个推进单元存在一个推进控制器,并且对于每个推进控制器存在一个IMU。当控制单元处存在故障时,每个推进控制单元被配置为自动生成命令并控制推进单元以试图稳定飞行器。

    An aerial vehicle may include a control unit configured to send control signals in order to control flight of the aerial vehicle, propulsion units configured to control the attitude of the aerial vehicle, propulsion controllers configured to send commands to a corresponding propulsion unit of the propulsion units based on the control signals, and inertial measurement units (IMU). Each of the IMUs is configured to provide attitude information to a corresponding one of the propulsion controllers. In this way, there is one propulsion controller for each of the propulsion units and one IMU for each of the propulsion controllers. When there is a failure at the control unit, each of the propulsion control unit units are configured automatically generate the commands and control the propulsion units in order to attempt to stabilize the aerial vehicle.


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    Titel :

    飞行器


    Erscheinungsdatum :

    2024-03-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen