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    CONTROL AND STABILIZATION OF A FLIGHT VEHICLE FROM A DETECTED PERTURBATION BY TILT AND ROTATION
    84.
    发明申请
    CONTROL AND STABILIZATION OF A FLIGHT VEHICLE FROM A DETECTED PERTURBATION BY TILT AND ROTATION 审中-公开
    通过倾斜和旋转从检测到的扰动控制和稳定飞行车辆

    公开(公告)号：US20160291598A1

    公开(公告)日：2016-10-06

    申请号：US15091566

    申请日：2016-04-05

    Applicant: THOMAS A. YOUMANS

    Inventor： THOMAS A. YOUMANS

    IPC: G05D1/08 ,  B64C13/18 ,  B64C27/08

    CPC classification number: G05D1/0816 ,  B64C17/02 ,  B64C19/00 ,  B64C27/00 ,  B64C27/08 ,  B64C29/00 ,  B64C39/024 ,  B64C39/026 ,  B64C2201/14 ,  G05D1/042 ,  G05D1/08 ,  G05D1/0808 ,  G05D1/0858

    Abstract: A flight vehicle control and stabilization process detects and measures an orientation of a non-fixed portion relative to a fixed frame or portion of a flight vehicle, following a perturbation in the non-fixed portion from one or both of tilt and rotation thereof. A pilot or rider tilts or rotates the non-fixed portion, or both, to intentionally adjust the orientation and effect a change in the flight vehicle's direction. The flight vehicle control and stabilization process calculates a directional adjustment of the rest of the flight vehicle from this perturbation and induces the fixed portion to re-orient itself with the non-fixed portion to effect control and stability of the flight vehicle. The flight vehicle control and stabilization process also detects changes in speed and altitude, and includes stabilization components to adjust flight vehicle operation from unintentional payload movement on the non-fixed portion.

    Abstract translation: 飞行器车辆控制和稳定过程在倾斜和旋转中的一个或两个的非固定部分中的扰动之后，检测并测量相对于固定框架或飞行器车辆的非固定部分的方位。 飞行员或骑手倾斜或旋转非固定部分或两者，有意调整方向并影响飞行器车辆方向的变化。 飞行器控制和稳定过程从该扰动计算飞行器的其余部分的方向调整，并且引起固定部分以使其与非固定部分重新定向以实现飞行器车辆的控制和稳定性。 飞行器控制和稳定过程还检测速度和高度的变化，并且包括稳定部件以通过非固定部分上的无意的有效载荷移动来调整飞行器操作。

    Utilizing acceleration information for precision landing of unmanned aerial vehicles
    86.
    发明授权
    Utilizing acceleration information for precision landing of unmanned aerial vehicles 有权
    利用无人机高精度着陆的加速度信息

    公开(公告)号：US09448562B1

    公开(公告)日：2016-09-20

    申请号：US14829226

    申请日：2015-08-18

    Applicant: Skycatch, Inc.

    Inventor： Behrooze Sirang ,  Stephan Brown

    IPC: G05D1/00 ,  G05D1/06 ,  B64C39/02

    CPC classification number: G05D1/0676 ,  B64C39/024 ,  B64C2201/14 ,  B64C2201/141 ,  B64C2201/18 ,  B64C2201/182 ,  B64C2201/201

    Abstract: Systems and methods disclosed utilize acceleration information in landing an unmanned aerial vehicle. In particular, one or more embodiments include methods and systems that determine a UAV is landing, identify an acceleration spike relative to the UAV, and modify operation of the UAV while landing based on the acceleration spike. For example, in one or more embodiment, systems and methods identify an acceleration spike, compare the acceleration spike to a pattern indicative of contact with another object, and reduce the rate of rotation of rotors utilized by the UAV for flight based on the comparison of the acceleration spike to the pattern.

    Abstract translation: 所公开的系统和方法利用登陆无人驾驶飞行器的加速度信息。 特别地，一个或多个实施例包括确定UAV着陆的方法和系统，识别相对于UAV的加速尖峰，以及基于加速尖峰而着陆时修改UAV的操作。 例如，在一个或多个实施例中，系统和方法识别加速尖峰，将加速度尖峰与指示与另一物体接触的模式进行比较，并且基于比较来降低无人机用于飞行的转子的旋转速率 加速飙升到图案。

    CLOUD-BASED CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLES
    87.
    发明申请
    CLOUD-BASED CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLES 审中-公开
    基于云的无人驾驶机动车控制系统

    公开(公告)号：US20160246297A1

    公开(公告)日：2016-08-25

    申请号：US15046560

    申请日：2016-02-18

    Applicant: Siemens Corporation

    Inventor： Zhen Song

    IPC: G05D1/00 ,  G08G5/00 ,  B64C39/02 ,  H04B7/185 ,  H04L29/08

    CPC classification number: G05D1/0022 ,  B64C39/024 ,  B64C2201/126 ,  B64C2201/14 ,  B64C2201/146 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/006 ,  G08G5/0069 ,  H04B7/18506 ,  H04L67/10 ,  H04L67/12 ,  H04W4/021

    Abstract: A cloud-based system for controlling the use of unmanned aerial vehicles (UAVs) is used as the communication path between a pilot and his/her UAV, eliminating the direct communication between pilot and vehicle. The cloud-basedUAV control system is configured to include both “control apps” associated with the actual flight of a UAV and “mission-specific apps” that include a set of instructions for a specific mission (i.e., performing energy audit of an industrial complex). The control apps preferably include flight regulations (as provided by the FAA, for example) that are used define “no-fly zones”. Other legitimate government (or non-government) agencies may provide “electric fence” control apps to the cloud-based system, thus preventing UAVs from entering protected areas. The UAVs interacting with the control system are intelligent, able to receive specific mission-based applications from the control system, allowing the UAVs to collect a wide variety of useful information.

    Abstract translation: 用于控制无人机（UAV）使用的基于云的系统被用作飞行员和他/她的UAV之间的通信路径，消除了飞行员和车辆之间的直接通信。 基于云的无人机控制系统被配置为包括与无人机的实际飞行相关联的“控制应用”和“任务特定应用”，其包括针对特定任务的一组指令（即，对工业进行能量审核 复杂）。 控制应用程序最好包括用于定义“禁止飞行区”的飞行规则（例如由FAA提供的）。 其他合法政府（或非政府机构）可以向云计算系统提供“电动围栏”控制应用程序，从而防止无人机进入保护区。 与控制系统交互的无人机是智能的，能够从控制系统接收特定的基于任务的应用，允许无人机收集各种有用的信息。

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