本发明涉及无人机技术领域,公开了一种飞行装置及飞行控制方法,所述飞行装置包括机翼系统、动力系统、感知系统和飞控系统;机翼系统沿机翼系统中轴线对称设置有多个安装位;动力系统包括若干动力模块,动力模块通过安装位挂载在机翼系统之上;感知系统用于感知安装位上是否安装有动力模块;飞控系统用于根据感知系统采集的动力信息调用飞控系统中对应的飞控子系统进行飞行控制,动力信息包括动力模块的安装位置和安装数量。本发明解决了用户无法针对任务需求自由调整飞行模块与飞行控制系统的组合形式的问题,提高了无人飞行装置的适用性。

    The invention relates to the technical field of unmanned aerial vehicles, and discloses a flight device and a flight control method. The flight device comprises a wing system, a power system, a sensing system and a flight control system; the wing system is symmetrically provided with a plurality of mounting positions along the central axis of the wing system; the power system comprises a plurality of power modules, and the power modules are mounted on the wing system through the mounting positions; the sensing system is used for sensing whether the power modules are mounted on the mounting positions; and the flight control system is used for calling a corresponding flight control subsystem in the flight control system to perform flight control according to the power information collected by the sensing system, and the power information comprises the mounting positions and the mounting number of the power modules. The problem that a user cannot freely adjust the combination form of the flight module and the flight control system according to task requirements is solved, and the applicability of the unmanned flight device is improved.


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    Title :

    飞行装置及飞行控制方法


    Publication date :

    2022-01-18


    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 / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen