首页> 外国专利> CONTROLLED FLIGHT OF A MULTICOPTER EXPERIENCING A FAILURE AFFECTING AN EFFECTOR

CONTROLLED FLIGHT OF A MULTICOPTER EXPERIENCING A FAILURE AFFECTING AN EFFECTOR

机译:经过影响效应器的失败的多个多板控制飞行

摘要

According to a first aspect of the invention, there is provided a method for iterating a multicopter experiencing a failure during flight, the multicopter comprising a body, and at least four effectors attached lo the body, each operable to produce both a torque and a thrust force which can cause the multicopter to fly when not experiencing said failure. The method may comprise the step of identifying a failure wherein the failure affects the torque and/or thrust force produced by an effector, and in response to identifying a failure carrying out the following steps, (1) computing an estimate of the orientation of a primary axis of said body with respect to a predefined reference frame, wherein said primary axis is an axis about which said multicopter rotates when living, (2) computing an estimate of the angular velocity of said multicopter, (3) controlling one or more of said at least four effectors based on said estimate of the orientation of the primary axis of said body with respect to said predefined reference frame and said estimate of the angular velocity of the multicopter. The step of controlling one or more of said ,u least four effectors may be performed such that (a) said one or mote electors collectively produce a torque along said primary axis and a torque perpendicular to said primary axis, wherein (i) the torque along said primary axis causes said multicopter to rotate about said primary axis, and (ii) the torque perpendicular to said primary axis causes said multicopter to move such that the orientation of said primary axis converges to a target orientation with respect to said predefined reference frame, and (b) such that said one or more effectors individually produce a thrust force along said primary axis.
机译:根据本发明的第一方面,提供了一种用于迭代在飞行期间经历故障的多功能的方法,包括主体的多个转换器,并且至少四个效应器附着在主体上,每个效应器都可以操作以产生扭矩和推力在不经历所述故障时可能导致多电位飞行的力。该方法可以包括识别故障的步骤,其中故障影响由执行器产生的扭矩和/或推力,并且响应于识别执行以下步骤的故障,(1)计算估计A的方向的估计所述主体的初级轴相对于预定的参考框架,其中所述初级轴是围绕该轴线围绕该轴线,(2)计算所述多变电器的角速度的估计,(3)控制一个或多个基于所述预定义参考框架的所述预定参考框架的主轴的方向的所述估计和所述多变速器角速度的所述估计,所述至少四个效应器。控制一个或多个所述的步骤,您可以执行至少四个效应器,使得(a)所述一个或电影选区沿着所述初级轴线共同产生扭矩和垂直于所述晶轴的扭矩,其中(i)扭矩沿着所述初级轴导致所述多变速器围绕所述初级轴旋转,并且(ii)垂直于所述初级轴的扭矩导致所述多变速器移动,使得所述初级轴的取向会收敛于相对于所述预定义参考帧的目标方向。 (B)使得所述一个或多个效应器单独地沿着所述初级轴产生推力。

著录项

  • 公开/公告号US2021188422A1

    专利类型

  • 公开/公告日2021-06-24

    原文格式PDF

  • 申请/专利权人 ETH ZURICH;

    申请/专利号US202117195744

  • 申请日2021-03-09

  • 分类号B64C13/24;B64C27/08;B64C27/20;B64C27/32;B64C39/02;B64D45;G05D1;

  • 国家 US

  • 入库时间 2022-08-24 19:32:19

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