The embodiment of the invention discloses a split type unmanned aerial vehicle, an unmanned aerial vehicle control system and a control method, and belongs to the technical field of unmanned aerial vehicles. A second body; a plurality of flight mechanisms are connected to the first fuselage, and a plurality of flight mechanisms are connected to the second fuselage; the connecting mechanism comprises a fixing part, a connecting arm and a fitting part which are connected in sequence; wherein the fixing part is connected with the first machine body, and the attaching part is detachably connected with the second machine body; and the undercarriage is connected with the second fuselage. Thus, through detachable connection between the attaching part and the second fuselage, detachable connection between the first fuselage and the second fuselage is achieved, when multiple target tasks need to be executed at the same time, the first fuselage and the second fuselage can be separated, and the first fuselage and the second fuselage execute the respective tasks respectively; and a single helicopter can execute a plurality of target tasks at the same time.
本申请的实施例公开了一种可分体式无人机、无人机控制系统及控制方法,属于无人机技术领域,该可分体式无人机包括:第一机身;第二机身;飞行机构,第一机身上连接有多个飞行机构,第二机身上连接有多个飞行机构;连接机构,连接机构包括依次连接的固定部、连接臂和贴合部;其中,固定部连接第一机身,贴合部与第二机身可拆卸连接;起落架,起落架与第二机身连接。如此,通过贴合部与第二机身的可拆卸连接,实现第一机身和第二机身之间的可拆卸连接,当需要同时执行多个目标任务时,可以将第一机身和第二机身分离,第一机身和第二机身分别执行各自的任务,实现单架直升机同时执行多个目标任务。
Split type unmanned aerial vehicle, unmanned aerial vehicle control system and control method
一种可分体式无人机、无人机控制系统及控制方法
25.08.2023
Patent
Elektronische Ressource
Chinesisch
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