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Drone, method for operating a drone and electronic control and regulating device for controlling and regulating the operation of a drone

机译:无人机,操作无人机和电子控制的方法,用于控制和调节无人机操作的控制

摘要

Drone (10) with a base structure (12) and at least three thrust generating devices (14a-d) arranged at different points in a horizontal plan view, which during operation generate a thrust with a thrust direction (28a-d) that is at least also vertically downwards directed thrust component, the thrust directions (28a-d) of at least two thrust generating devices (14a-d) being pivotable relative to the base structure (14) independently of one another during flight, characterized in that the base structure (12) is elongated and thus in Has a comparatively small cross section in the direction of a longitudinal axis (16), that the base structure (12) has a longitudinal axis (16), that on the base structure (12) a bracket (32) extending in a longitudinal direction (16) of the base structure (12) is arranged, and that the thrust directions (28a-d) are each pivotable about an axis (22a-d) which is orthogonal to the longitudinal axis (16).
机译:具有基座结构(12)的无人机(10)和至少三个推力产生装置(14a-d)布置在水平平面图中的不同点,在操作期间产生具有推力方向(28a-d)的推力 至少还垂直向下的指向推力部件,至少两个推力产生装置(14a-d)的推力方向(28a-d)可相对于基础结构(14)在飞行期间彼此独立地枢转,其特征在于 基部结构(12)伸长,因此在纵向轴线(16)的方向上具有相对小的横截面,即基部结构(12)具有纵向轴线(16),在基座结构(12)上 布置在基部结构(12)的纵向(16)中延伸的支架(32)被布置,并且推力方向(28a-d)围绕与纵向正交的轴(22a-d)可枢转 轴(16)。

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