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公开(公告)号：US20160332739A1
公开(公告)日：2016-11-17
申请号：US14713343
申请日：2015-05-15
Applicant: Disney Enterprises, Inc.
Inventor： Clifford Wong
CPC classification number: B64D25/00 , B64C39/00 , B64C39/024 , B64C2201/00 , B64C2201/024 , B64C2201/14 , B64C2201/146 , B64C2201/18 , B64C2201/185
Abstract: An unmanned aerial vehicle apparatus comprises a frame. Further, the unmanned aerial vehicle apparatus comprises a propulsion mechanism coupled to the frame that propels the frame through the air. In addition, the unmanned aerial vehicle apparatus comprises a storage device that stores one or more airbags and is coupled to the frame. The unmanned aerial vehicle apparatus also comprises an inflation device coupled to the frame that receives an activation signal and inflates the one or more airbags based upon receipt of the activation signal to deploy the one or more airbags from the storage device prior to an impact of the frame with an object.
Abstract translation: 无人驾驶飞行器装置包括一个框架。 此外，无人驾驶飞行器装置包括联接到框架的推进机构，其推动框架通过空气。 此外，无人驾驶飞行器装置包括存储装置，该存储装置存储一个或多个安全气囊并且联接到该框架。 无人驾驶飞行器装置还包括联接到框架的充气装置，其接收启动信号，并且基于接收到激活信号而使一个或多个安全气囊充气，以在所述启动信号的影响之前从所述存储装置部署所述一个或多个气囊 框架与对象。
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132.发明授权System and method for placement of sensors through use of unmanned aerial vehicles 有权使用无人驾驶飞行器放置传感器的系统和方法公开(公告)号：US09454907B2
公开(公告)日：2016-09-27
申请号：US14716850
申请日：2015-05-19
Applicant: Usman Hafeez , David Mauer
Inventor： Usman Hafeez , David Mauer
CPC classification number: G08G5/0034 , B64C39/024 , B64C2201/00 , B64C2201/027 , B64C2201/12 , G01C21/20 , G05D1/104 , G08G5/0043 , G08G5/0069
Abstract: The invention is directed toward a system and method for placing, activating, and testing sensors. The system comprises one or more server computers, one or more communication hubs, one or more unmanned aerial vehicles, and one or more sensors. The method comprises the steps of receiving geographic sensor placement locations, receiving sensor parameters, determining the geographic location of sensors, respectively sending location query signals to the unmanned aerial vehicles, respectively receiving location reply signals from the unmanned aerial vehicles, and calculating a geographic flight path for the unmanned aerial vehicles. The method also comprises calculating mission objectives and the energy needs of the unmanned aerial vehicles to complete the mission objectives. The method then determines the most efficient combination of unmanned aerial vehicles to complete the mission objectives and assigns the tasks to the unmanned aerial vehicles. The unmanned aerial vehicles place, activate, and test the sensors.
Abstract translation: 本发明涉及用于放置，激活和测试传感器的系统和方法。 该系统包括一个或多个服务器计算机，一个或多个通信集线器，一个或多个无人驾驶飞行器以及一个或多个传感器。 该方法包括以下步骤：接收地理传感器放置位置，接收传感器参数，确定传感器的地理位置，分别向无人驾驶飞行器发送位置查询信号，分别接收来自无人机的位置应答信号，以及计算地理飞行 无人机的路径。 该方法还包括计算任务目标和无人机的能源需求，以完成任务目标。 然后，该方法确定无人机的最有效的组合来完成任务目标并将任务分配给无人驾驶飞行器。 无人驾驶飞行器放置，激活和测试传感器。
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133.发明申请SYSTEM AND METHOD FOR PLACEMENT OF SENSORS THROUGH USE OF UNMANNED AERIAL VEHICLES 审中-公开通过使用无人驾驶飞机放置传感器的系统和方法公开(公告)号：US20160232794A1
公开(公告)日：2016-08-11
申请号：US14716850
申请日：2015-05-19
Applicant: Usman Hafeez , David Mauer
Inventor： Usman Hafeez , David Mauer
CPC classification number: G08G5/0034 , B64C39/024 , B64C2201/00 , B64C2201/027 , B64C2201/12 , G01C21/20 , G05D1/104 , G08G5/0043 , G08G5/0069
Abstract: The invention is directed toward a system and method for placing, activating, and testing sensors. The system comprises one or more server computers, one or more communication hubs, one or more unmanned aerial vehicles, and one or more sensors. The method comprises the steps of receiving geographic sensor placement locations, receiving sensor parameters, determining the geographic location of sensors, respectively sending location query signals to the unmanned aerial vehicles, respectively receiving location reply signals from the unmanned aerial vehicles, and calculating a geographic flight path for the unmanned aerial vehicles. The method also comprises calculating mission objectives and the energy needs of the unmanned aerial vehicles to complete the mission objectives. The method then determines the most efficient combination of unmanned aerial vehicles to complete the mission objectives and assigns the tasks to the unmanned aerial vehicles. The unmanned aerial vehicles place, activate, and test the sensors.
Abstract translation: 本发明涉及用于放置，激活和测试传感器的系统和方法。 该系统包括一个或多个服务器计算机，一个或多个通信集线器，一个或多个无人驾驶飞行器以及一个或多个传感器。 该方法包括以下步骤：接收地理传感器放置位置，接收传感器参数，确定传感器的地理位置，分别向无人驾驶飞行器发送位置查询信号，分别接收来自无人机的位置应答信号，以及计算地理飞行 无人机的路径。 该方法还包括计算任务目标和无人机的能源需求，以完成任务目标。 然后，该方法确定无人机的最有效的组合来完成任务目标并将任务分配给无人驾驶飞行器。 无人驾驶飞行器放置，激活和测试传感器。
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公开(公告)号：US09409644B2
公开(公告)日：2016-08-09
申请号：US14333462
申请日：2014-07-16
Applicant: Ford Global Technologies, LLC
Inventor： Joseph F. Stanek , John A. Lockwood
CPC classification number: G05D1/0276 , B60R16/02 , B60W30/00 , B64C29/0008 , B64C29/0091 , B64C29/02 , B64C39/00 , B64C39/02 , B64C39/022 , B64C39/024 , B64C2201/00 , B64C2201/02 , B64C2201/08 , B64C2201/086 , B64C2201/088 , B64C2201/12 , B64C2201/126 , B64C2201/127 , B64C2201/14 , B64C2201/141 , B64C2201/18 , B64C2201/182 , B64C2201/185 , B64C2201/187 , B64C2201/20 , B64C2201/208 , B64C2230/00 , G05D1/0022 , G05D1/0088 , G05D1/0094 , G05D1/0202 , G05D1/0212 , G05D1/0231 , G05D1/0242 , G05D1/0255 , G05D1/0257 , G05D1/028 , G05D2201/0213 , G08C17/00 , G08G1/012 , G08G1/091
Abstract: This disclosure generally relates to an automotive drone deployment system that includes at least a vehicle and a deployable drone that is configured to attach and detach from the vehicle. More specifically, the disclosure describes the vehicle and drone remaining in communication with each other to exchange information while the vehicle is being operated in an autonomous driving mode so that the vehicle's performance under the autonomous driving mode is enhanced.
Abstract translation: 本公开总体上涉及一种汽车无人机部署系统，该系统至少包括车辆和可部署的无人机，其配置为从车辆附接和分离。 更具体地，本公开描述了当车辆以自主驾驶模式操作时彼此保持通信的车辆和无人机交换信息，使得车辆在自主驾驶模式下的性能得到增强。
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135.发明申请METHOD AND SYSTEM FOR ESTIMATING INFORMATION RELATED TO A VEHICLE PITCH AND/OR ROLL ANGLE 有权用于估计与车辆倾斜角和/或角度角相关的信息的方法和系统公开(公告)号：US20150323648A1
公开(公告)日：2015-11-12
申请号：US14362767
申请日：2014-04-14
Applicant: SAAB Vricon Systems AB
Inventor： Leif Haglund , Folke Isaksson , Michael Felsberg , Bertil Grelsson
CPC classification number: G01S5/163 , B64C2201/00 , G01C9/06 , G01C11/00 , G01C15/14 , G01C21/005 , G01C21/20 , G01S17/06 , G06T7/80 , G06T2207/10016 , G06T2207/10024 , G06T2207/20061 , G06T2207/30244 , G06T2207/30252 , G09B9/48
Abstract: The present disclosure relates to a method (200) for estimating information related to a vehicle pitch and/or roll angle. The method comprises a step of obtaining (220) a first estimate of the information related to the pitch and/or roll angle. The method is characterized by the steps of capturing (210) an image of an area covering at least a part of the horizon using a camera mounted on the airborne vehicle, and determining (240) an improved estimate of the information related to the pitch and/or roll angle based on the first estimate of the information related to the pitch and/or roll angle, and a digital elevation model.
Abstract translation: 本公开涉及一种用于估计与车辆俯仰和/或侧倾角相关的信息的方法（200）。 该方法包括获得（220）与俯仰和/或倾斜角相关的信息的第一估计的步骤。 该方法的特征在于以下步骤：使用安装在机载车上的照相机捕获（210）覆盖至少一部分水平线的区域的图像，并且确定（240）对与音高有关的信息的改进估计， /或基于与俯仰角和/或侧倾角相关的信息的第一估计的滚角，以及数字高程模型。
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Patent Agency Ranking
公开(公告)号：US09146557B1
公开(公告)日：2015-09-29
申请号：US14260096
申请日：2014-04-23
Inventor： Ghufran Ahmed , Sami El Ferik
IPC: B64C19/00 , B64C17/00 , B64B1/20 , G05D1/08 , G05D1/10 , G05D1/00 , B64D9/00 , B64C39/02 , B64D1/22
CPC classification number: G05D1/10 , B64C17/00 , B64C19/00 , B64C39/024 , B64C2201/00 , B64C2201/024 , B64C2201/128 , B64C2201/14 , B64D1/22 , G05B13/04 , G05D1/08 , G05D1/0808 , G05D1/0816 , G05D1/0825 , G05D1/085 , G05D1/0858 , G05D1/101
Abstract: The adaptive control method for an unmanned vehicle with a slung load utilizes a feedback linearization controller (FLC) to perform vertical take off, hovering and landing of an unmanned aerial vehicle with a slung load, such as a quadrotor drone or the like. The controller includes a double loop architecture, where the overall controller includes an inner loop having an inner controller which is responsible for controlling the attitude angles and the altitude, and an outer loop having an outer controller responsible for providing the inner loop inner controller with the desired angle values. States, such as including roll, pitch, yaw and/or altitude, are selected as outputs and the feedback linearization technique is used.
Abstract translation: 具有悬挂载荷的无人驾驶车辆的自适应控制方法利用反馈线性化控制器（FLC）来执行具有诸如四旋翼无人机等的悬挂载荷的无人驾驶飞行器的垂直起飞，悬停和着陆。 该控制器包括一个双回路结构，其中总体控制器包括一个具有负责控制姿态角度和高度的内部控制器的内部回路，以及一个外部控制器，该外部控制器负责向内部循环内部控制器提供 所需的角度值。 选择诸如滚动，俯仰，偏航和/或高度的状态作为输出，并且使用反馈线性化技术。
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公开(公告)号：US20150160658A1
公开(公告)日：2015-06-11
申请号：US14310307
申请日：2014-06-20
Applicant: BCB INTERNATIONAL LTD. , TORQUING GROUP LTD.
Inventor： Ivan Reedman , Barry Davies
CPC classification number: B64C39/024 , B64C19/00 , B64C39/028 , B64C2201/00 , B64C2201/14 , B64C2201/141 , B64C2230/00 , B64C2230/02 , G01S15/06 , G01S15/88 , G01S15/89 , G01S15/8913 , G01S15/8929 , G01S15/8993 , G01S15/93 , G05D1/0088 , G05D1/0202 , G05D1/101 , G05D1/102 , Y10S367/909
Abstract: A micro unmanned aerial vehicle or drone (“UAV”) 10 is remotely controlled through an HMI, although this remote control is supplemented by and selectively suppressed by an on-board controller. The controller operates to control the generation of a sonar bubble that generally encapsulates the UAV. The sonar bubble, which may be ultrasonic in nature, is produced by a multiplicity of sonar lobes generated by specific sonar emitters associated with each axis of movement for the UAV. The emitters produce individual and beamformed sonar lobes that partially overlap to provide stereo or bioptic data in the form of individual echo responses detected by axis-specific sonar detectors. In this way, the on-board controller is able to interpret and then generate 3-D spatial imaging of the physical environment in which the UAV is currently moving or positioned. The controller is therefore able to plot relative and absolute movement of the UAV through the 3-D space by recording measurements from on-board gyroscopes, magnetometers and accelerometers. Data from the sonar bubble can therefore both proactively prevent collisions with objects by imposing a corrective instruction to rotors and other flight control system and can also assess and compensate for sensor drift.
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公开(公告)号：US20120160959A1
公开(公告)日：2012-06-28
申请号：US13342373
申请日：2012-01-03
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
IPC: B64B1/00
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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公开(公告)号：US20080179454A1
公开(公告)日：2008-07-31
申请号：US11907883
申请日：2007-10-18
Applicant: Pierre Balaskovic
Inventor： Pierre Balaskovic
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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公开(公告)号：US1203383A
公开(公告)日：1916-10-31
申请号：US7572416
申请日：1916-02-02
Applicant: JAMES E NORRIS , MILLICAN JOEL W
Inventor： MILLICAN JOEL W
CPC classification number: B64C2201/00
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