The invention discloses a control method of a combined unmanned aerial vehicle, relates to the field of unmanned aerial vehicle control, and particularly relates to a multi-degree-of-freedom vector combined unmanned aerial vehicle. In order to solve problems in the prior art, the unmanned aerial vehicle shows different properties in different combination modes, and after combination, the unmanned aerial vehicle can hover and fly at any angle so that the unmanned aerial vehicle can pass through some narrow spaces, the load of the unmanned aerial vehicle is increased, and a single module can also work independently. Through an unmanned aerial vehicle real-time modeling technology, unmanned aerial vehicles can be combined in the air. By splitting and combining in the air and changing the number and the combination mode of the combined unmanned aerial vehicles, the purposes of improving the degree of freedom, improving the load and freely coping with the narrow environment are achieved, meanwhile, when the number of the combined modules is large, after a certain module power device breaks down, the controller can control the stable flight of the whole combination through a control algorithm, and the safety performance of the unmanned aerial vehicle is improved.

    本发明公开了一种组合式无人机的控制方法,涉及无人机控制领域,特别涉及多自由度矢量组合式无人机。针对上述现有技术中存在的问题,本发明在不同的组合方式下,无人机表现出不同的性质,在组合后,无人机可以进行任意角度悬停飞行,有助于通过一些狭小的空间,增加无人机载重,而单个模块也能独立工作。通过无人机实时建模技术,可以实现无人机在空中进行组合。本发明通过在空中进行拆分组合,改变组合无人机的数目和组合方式,来达到提高自由度,提高负载,自由应对狭窄环境的目的,同时当组合的模块较多时,某个模块动力器件发生故障后,控制器能够通过控制算法来控制组合整体的稳定飞行,提高了无人机的安全性能。


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    Titel :

    Control method of combined unmanned aerial vehicle


    Weitere Titelangaben:

    一种组合式无人机的控制方法


    Beteiligte:
    LI FUSHENG (Autor:in) / WU ZEGUI (Autor:in) / ZHANG WEIYE (Autor:in) / YE JUNTING (Autor:in)

    Erscheinungsdatum :

    2021-04-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge





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