会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 3. 发明授权
    • Remote control system and method and usage related to such a system
    • 遥控系统及与此类系统相关的方法和用法
    • US09529358B2
    • 2016-12-27
    • US14441016
    • 2013-11-01
    • KVASER AB
    • Lars-Berno Fredriksson
    • A63H30/04H04L12/40B64C39/00G05D1/00B64C39/02
    • G05D1/0016A63H30/04B64C39/024B64C2201/146B64C2203/00
    • The invention relates to a remote control system (195) comprising mobile units (190, 1102, 1105), and a by control means (106, 110) provided controller unit for these. Said units are equipped with a function performing means (161) and transferring means (207, 270) that generates information signals (301) respectively transmits the same. Signal processing means (261, 268) and their exerting function (314) for controlling the functions of the respective mobile unit are placed respectively takes place only in the current mobile device. In accordance with the proposed use in connection with the present invention object, a controller area network type of system is constructed with a distributed and integrated network structure (1751). Only signal processing means (1753) and their function exertion means (1754) for controlling of a mobile unit, which is positioned in the actual unit, is used for its control. According to the method establishes a structure of a controller area network type with modular units (1753′), nodes (1753) and a communication protocol (501) for the node communication. All messages transmitted by the nodes are received by the modular units (1754, 1792). A information comparison (1755, 176) is used to select respective message or part thereof.
    • 本发明涉及包括移动单元(190,1102,1105)的远程控制系统(195),以及由这些控制装置(106,110)提供的控制单元。 所述单元配备有产生信息信号(301)的功能执行装置(161)和传送装置(207,270),分别传送它们。 信号处理装置(261,268)及其用于控制​​各个移动单元的功能的作用功能(314)分别仅在当前的移动装置中进行。 根据本发明目的的提出的使用,系统的控制器区域网络类型由分布式和集成的网络结构构成(1751)。 仅用于控制位于实际单元中的移动单元的信号处理装置(1753)及其功能消耗装置(1754)用于其控制。 根据该方法建立了具有用于节点通信的模块单元(1753'),节点(1753)和通信协议(501)的控制器区域网络类型的结构。 由节点发送的所有消息都由模块单元(1754,1792)接收。 信息比较(1755,176)用于选择相应的消息或其一部分。
    • 5. 发明申请
    • CONTROLLED FLIGHT OF A MULTICOPTER EXPERIENCING A FAILURE AFFECTING AN EFFECTOR
    • 经营影响影响的故障的多功能人员的控制飞行
    • US20160107751A1
    • 2016-04-21
    • US14893874
    • 2014-06-05
    • ETH ZURICH
    • Raffaello D'ANDREASergei LUPASHINMark W. MUELLERMarkus WAIBEL
    • B64C39/02B64D45/00B64C27/08
    • B64C13/24B64C27/08B64C27/20B64C27/32B64C39/024B64C2201/024B64C2201/027B64C2201/108B64C2201/127B64C2201/141B64C2201/146B64C2203/00B64D45/00G05D1/0072
    • According to a first aspect of the invention, there is provided a method for operating a multicopter experiencing a failure during flight, the multicopter comprising a body, and at least four effectors attached to 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 flying, (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 at least four effectors may be performed such that (a) said one or more effectors 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.
    • 根据本发明的第一方面,提供了一种用于操作在飞行期间经历故障的多机器的方法,所述多机器包括主体,以及附接到所述主体的至少四个执行器,每个可操作以产生扭矩和推力 在不经历所述故障时可能导致多机器飞行的力。 该方法可以包括识别故障的步骤,其中故障影响由效应器产生的扭矩和/或推力,并且响应于识别执行以下步骤的故障,(1)计算一个 所述主体相对于预定义的参考框架的主轴线,其中所述主轴线是所述多机器在飞行时旋转的轴线,(2)计算所述多机器的角速度的估计,(3)控制一个或多个 基于所述身体的主轴的方向相对于所述预定参考框架的所述估计和所述多机器的角速度的估计,至少四个效应器。 可以执行控制所述至少四个效应器中的一个或多个的步骤,使得(a)所述一个或多个效应器共同地沿着所述主轴产生扭矩和垂直于所述主轴的扭矩,其中(i)沿着 所述主轴使所述多机器人围绕所述主轴线旋转,并且(ii)垂直于所述主轴线的转矩使得所述多机器人移动,使得所述主轴线的方向相对于所述预定参考系收敛到目标方位, 和(b)使得所述一个或多个效应器单独地沿着所述主轴产生推力。