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    SENSOR CALIBRATION SYSTEM
    111.
    发明申请
    SENSOR CALIBRATION SYSTEM 有权
    传感器校准系统

    公开(公告)号：US20160245899A1

    公开(公告)日：2016-08-25

    申请号：US15143150

    申请日：2016-04-29

    Applicant: Caterpillar Inc.

    Inventor： Paul Edmund Rybski

    IPC: G01S7/40 ,  B64F5/00 ,  G06T7/00 ,  B64C39/02 ,  G01S7/497 ,  G01S7/52

    CPC classification number: G01S7/4004 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/027 ,  B64C2201/12 ,  G01S7/4026 ,  G01S7/497 ,  G01S7/52004 ,  G01S2007/403 ,  G01S2007/4034 ,  G01S2007/4091 ,  G05D1/102 ,  G06T2207/10032 ,  G06T2207/30252

    Abstract: A calibration system for a machine is provided. The calibration system includes an unmanned aerial vehicle provided in association with a perception sensor. The unmanned aerial vehicle includes a target attached thereto. The unmanned aerial vehicle is configured to move along a predetermined path sweeping across a field of view of the perception sensor. The unmanned aerial vehicle is configured to present the target to the perception sensor, such that the target covers the field of view of the perception sensor based on the movement of the unmanned aerial vehicle along the predetermined path. The unmanned aerial vehicle is configured to determine and communicate an orientation and a position of the target to the calibration system.

    Abstract translation: 提供了一种用于机器的校准系统。 校准系统包括与感知传感器相关联地提供的无人驾驶飞行器。 无人飞行器包括附接到其上的目标。 无人驾驶飞行器构造成沿着穿过感知传感器的视野扫掠的预定路径移动。 无人驾驶飞行器被配置为将目标呈现给感知传感器，使得目标基于无人驾驶飞行器沿着预定路径的移动来覆盖感知传感器的视场。 无人驾驶飞行器被配置为确定并将目标的定向和位置传达到校准系统。

    ULTRALIGHT AIRCRAFT
    112.
    发明申请
    ULTRALIGHT AIRCRAFT 审中-公开
    ULTRALIGHT飞机

    公开(公告)号：US20160236789A1

    公开(公告)日：2016-08-18

    申请号：US15041424

    申请日：2016-02-11

    Applicant: AIRBUS DEFENCE AND SPACE GMBH

    Inventor： Simon BURNS

    IPC: B64D27/02 ,  B64C39/02 ,  B64C31/00

    CPC classification number: B64D27/02 ,  B64C31/00 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/165

    Abstract: An aircraft which has a supporting structure which has at least one fuselage, a wing structure and at least one drive apparatus. The drive apparatus has at least one propeller and a drive motor. The aircraft has at least one energy store for providing energy for operation of the drive apparatus. The at least one drive apparatus and the at least one energy store are mechanically connected to the supporting structure and/or the wing structure of the aircraft by a securing device.

    Abstract translation: 具有至少一个机身，机翼结构和至少一个驱动装置的支撑结构的飞机。 驱动装置具有至少一个螺旋桨和驱动马达。 飞机具有至少一个能量存储器，用于为驱动装置的操作提供能量。 所述至少一个驱动装置和所述至少一个能量存储器通过固定装置机械连接到所述飞行器的支撑结构和/或机翼结构。

    Projection assemblies for use with unmanned aerial vehicles
    113.
    发明授权
    Projection assemblies for use with unmanned aerial vehicles 有权
    用于无人机的投影组件

    公开(公告)号：US09405181B2

    公开(公告)日：2016-08-02

    申请号：US14448777

    申请日：2014-07-31

    Applicant: DISNEY ENTERPRISES, INC.

    Inventor： Clifford W. Wong ,  Michael J. Ilardi

    IPC: G03B21/56 ,  G03B37/00 ,  G03B21/10 ,  G03B21/62 ,  G03B21/28

    CPC classification number: G03B21/56 ,  B64C2201/00 ,  B64C2201/123 ,  G03B21/10 ,  G03B21/28 ,  G03B21/562 ,  G03B21/565 ,  G03B21/567 ,  G03B21/62 ,  G03B37/00 ,  G03B37/06

    Abstract: A projection assembly for use with an unmanned aerial vehicle (UAV) such as quadrotors. The projection assembly includes a projection screen with a rear surface and a front surface, and the projection screen has a level of opacity and/or other physical qualities that enables it to function as a rear-projection surface. The projection assembly includes a vehicle attachment member adapted for coupling with a frame of the UAV, and the projection screen is supported at a first end by the vehicle attachment member. The apparatus includes a projector projecting light, and the projected light is directed onto the rear surface of the projection surface to generate a displayed image visible on the front surface. The projection screen can be formed from a mesh sheet with a porosity allowing air to flow through the projection screen. The mesh sheet may be formed of plastic threads that provide the rear-projection surface function.

    Abstract translation: 一种与无人驾驶飞行器（UAV）一起使用的投影组件，如四旋转。 投影组件包括具有后表面和前表面的投影屏幕，并且投影屏幕具有使其能够用作后投影表面的不透明度和/或其他物理质量的水平。 所述突起组件包括适于与所述UAV的框架联接的车辆附接构件，并且所述投影屏幕在第一端处被所述车辆附接构件支撑。 该装置包括投影仪投射光，并且投影光被引导到投影表面的后表面上以产生在前表面上可见的显示图像。 投影屏幕可以由具有允许空气流过投影屏幕的孔隙的网片形成。 网片可以由提供后投影表面功能的塑料线形成。

    COMMUNITY DRONE MONITORING AND INFORMATION EXCHANGE
    114.
    发明申请
    COMMUNITY DRONE MONITORING AND INFORMATION EXCHANGE 有权
    社区监督和信息交流

    公开(公告)号：US20160180719A1

    公开(公告)日：2016-06-23

    申请号：US14581881

    申请日：2014-12-23

    Applicant: Intel Corporation

    Inventor： Rita H. Wouhaybi ,  Hong Li ,  Tobias Kohlenberg ,  Igor Tatourian

    IPC: G08G5/00 ,  B64C39/02

    CPC classification number: G08G5/0082 ,  B64C39/024 ,  B64C2201/00 ,  G06K9/00624 ,  G06K9/0063 ,  G08G5/0004 ,  G08G5/0026 ,  G08G5/0034 ,  G08G5/006 ,  G08G5/0069

    Abstract: A method may include receiving, using at least one processor, location information that includes a location of an unmanned aerial vehicle (UAV); querying, using the at least one processor, a policy database to retrieve a notification condition for a first property with respect to UAVs; calculating, using the at least one processor, a distance between the UAV and the first property using the received location information determining, using the at least one processor, if the distance of the UAV with respect to the first property is within a range defined in the notification condition for the first property; and transmitting, using the at least one processor, a notification to a party associated with the first property when the distance of the UAV with respect to the first property is within the range defined in the notification condition for the first property.

    Abstract translation: 一种方法可以包括：使用至少一个处理器来接收包括无人机（UAV）的位置的位置信息; 使用所述至少一个处理器查询策略数据库来检索关于UAV的第一属性的通知条件; 使用所接收的位置信息，使用所述至少一个处理器计算所述UAV和所述第一属性之间的距离，使用所述至少一个处理器来确定所述UAV相对于所述第一属性的距离是否在 第一财产的通知条件; 以及当所述UAV相对于所述第一属性的距离在所述第一属性的所述通知条件中限定的范围内时，使用所述至少一个处理器向与所述第一属性相关联的方发送通知。

    Apparatus for use on unmanned vehicles
    115.
    发明授权
    Apparatus for use on unmanned vehicles 有权
    用于无人驾驶车辆的装置

    公开(公告)号：US09156552B2

    公开(公告)日：2015-10-13

    申请号：US14129195

    申请日：2012-06-20

    Applicant: Isobel Louise Freeman ,  Keith Antony Rigby

    Inventor： Isobel Louise Freeman ,  Keith Antony Rigby

    IPC: G05D1/00 ,  B64C39/02 ,  F41H7/00 ,  F41H13/00 ,  F42B12/36

    CPC classification number: B64C39/024 ,  B64C2201/00 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/127 ,  F41H7/005 ,  F41H13/00 ,  F42B12/365

    Abstract: An apparatus, and a method performed by the apparatus, are disclosed wherein the apparatus can be mounted on an unmanned vehicle and arranged to act upon a payload. The payload can be mounted on the unmanned vehicle and, under an action of the apparatus, is able to be activated. The method can include receiving an activation instruction from an entity remote from the unmanned vehicle; determining whether or not the received activation instruction is valid by performing a validation process; and in response to determining that the received activation instruction is valid, activating the payload. In response to determining that the received activation instruction is not valid, activation of the payload may be prevented or opposed.

    Abstract translation: 公开了一种装置和由该装置执行的方法，其中该装置可以安装在无人驾驶车辆上并被布置为作用在有效载荷上。 有效载荷可以安装在无人驾驶车辆上，并且在装置的作用下能够被激活。 该方法可以包括从远程无人驾驶车辆的实体接收激活指令; 通过执行验证过程来确定所接收到的激活指令是否有效; 并且响应于确定所接收到的激活指令是有效的，激活有效载荷。 响应于确定接收到的激活指令无效，可以防止或反对有效载荷的激活。

    Lenticular airship
    118.
    发明授权
    Lenticular airship 有权
    透镜飞艇

    公开(公告)号：US08418952B2

    公开(公告)日：2013-04-16

    申请号：US13342373

    申请日：2012-01-03

    Applicant: Pierre Balaskovic

    Inventor： Pierre Balaskovic

    IPC: B64B1/12 ,  B64B1/10

    CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

    Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

    LENTICULAR AIRSHIP
    119.
    发明申请
    LENTICULAR AIRSHIP 有权
    航空公司

    公开(公告)号：US20110163200A1

    公开(公告)日：2011-07-07

    申请号：US12957989

    申请日：2010-12-01

    Applicant: Pierre Balaskovic

    Inventor： Pierre Balaskovic

    IPC: B64B1/06 ,  B64B1/22 ,  B64B1/24 ,  B64B1/12

    CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

    Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

    Lenticular airship
    120.
    发明授权
    Lenticular airship 有权
    透镜飞艇

    公开(公告)号：US07866601B2

    公开(公告)日：2011-01-11

    申请号：US11907883

    申请日：2007-10-18

    Applicant: Pierre Balaskovic

    Inventor： Pierre Balaskovic

    IPC: B64B1/12 ,  B64B1/10

    CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

    Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

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