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公开(公告)号：US08931730B2
公开(公告)日：2015-01-13
申请号：US14167679
申请日：2014-01-29
Applicant: SZ DJI Technology Co., Ltd
Inventor： Tao Wang , Tao Zhao , Hao Du , Mingxi Wang
CPC classification number: B64C1/063 , A63H27/12 , B64C1/00 , B64C1/061 , B64C25/32 , B64C27/08 , B64C39/024 , B64C39/028 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64D47/00 , B64D47/08 , G05D1/042
Abstract: Systems, devices, and methods for a transformable aerial vehicle are provided. In one aspect, a transformable aerial vehicle includes: a central body and at least two transformable frames assemblies respectively disposed on the central body, each of the at least two transformable frame assemblies having a proximal portion pivotally coupled to the central body and a distal portion; an actuation assembly mounted on the central body and configured to pivot the at least two frame assemblies to a plurality of different vertical angles relative to the central body; and a plurality of propulsion units mounted on the at least two transformable frame assemblies and operable to move the transformable aerial vehicle.
Abstract translation: 提供了可变形飞行器的系统，装置和方法。 一方面，可变形飞行器包括：中心体和分别设置在中心体上的至少两个可变形框架组件，所述至少两个可变形框架组件中的每一个具有枢转地联接到中心体的近侧部分和远端部分 ; 驱动组件，其安装在所述中心主体上并且构造成将所述至少两个框架组件相对于所述中心体枢转到多个不同的垂直角度; 以及安装在所述至少两个可变形框架组件上并可操作以移动所述可变形飞行器的多个推进单元。
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102.发明授权Multi-part navigation process by an unmanned aerial vehicle for navigating to a medical situatiion 有权用于导航到医疗状况的无人机的多部分导航过程公开(公告)号：US08930044B1
公开(公告)日：2015-01-06
申请号：US13730317
申请日：2012-12-28
Applicant: Google Inc.
Inventor： Eric Peeters , Eric Teller , William Graham Patrick
CPC classification number: G05D1/00 , B64C19/00 , B64C39/024 , B64C2201/12 , B64C2201/14 , B64C2201/145 , B64C2201/146 , G01S5/00 , G01S5/02 , G01S13/882 , G01S13/9303 , G01S13/94 , G01S15/93 , G01S17/933 , G05D1/12 , G08G5/0069
Abstract: Embodiments described herein may relate to an unmanned aerial vehicle (UAV) navigating to a medical situation in order to provide medical support. An illustrative method involves a UAV (a) determining an approximate target location associated with a medical situation, (b) using a first navigation process to navigate the UAV to the approximate target location, where the first navigation process generates flight-control signals based on the approximate target location, (c) making a determination that the UAV is located at the approximate target location, and (d) in response to the determination that the UAV is located at the approximate target location, using a second navigation process to navigate the UAV to the medical situation, wherein the second navigation process generates flight-control signals based on real-time localization of the medical situation.
Abstract translation: 本文描述的实施例可以涉及导航到医疗情况以便提供医疗支持的无人驾驶飞行器（UAV）。 一种说明性方法涉及UAV（a）确定与医疗状况相关联的近似目标位置，（b）使用第一导航过程将UAV导航到近似目标位置，其中第一导航过程基于 近似目标位置，（c）确定UAV位于大致目标位置，以及（d）响应于UAV位于大致目标位置的确定，使用第二导航处理来导航 无人机到医疗情况，其中第二导航过程基于医疗情况的实时定位产生飞行控制信号。
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公开(公告)号：US20180356822A1
公开(公告)日：2018-12-13
申请号：US16051481
申请日：2018-07-31
Applicant: AeroVironment, Inc.
Inventor： William J. Nicoloff , Eric M. Sornborger , Lars B. Cremean
CPC classification number: G05D1/0094 , B64C9/00 , B64C39/024 , B64C2201/021 , B64C2201/121 , B64C2201/123 , B64C2201/14 , B64D47/08 , F41G7/2253 , F41G7/2293 , F41G7/30
Abstract: An aircraft including a wing system, a plurality of control surfaces, a camera mounted on a camera pod, and a control system. The camera pod is configured to vary the orientation of the camera field of view only in yaw, relative to the aircraft, between a directly forward-looking orientation and a side-looking orientation. The control system controls the control surfaces such that they induce a significant aircraft yaw causing an identified target to be within the field of view of the camera with the camera in the directly forward-looking orientation.
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公开(公告)号：US20180307223A1
公开(公告)日：2018-10-25
申请号：US15785212
申请日：2017-10-16
Applicant: X Development LLC
Inventor： Eric Peeters , Eric Teller , William Graham Patrick
IPC: G05D1/00 , G08G5/00 , B64C19/00 , G05D1/12 , B64C39/02 , G01S5/02 , G01S13/93 , G01S13/88 , G01S5/00 , G01S17/93 , G01S13/94 , G01S15/93
CPC classification number: G05D1/00 , B64C19/00 , B64C39/024 , B64C2201/12 , B64C2201/14 , B64C2201/145 , B64C2201/146 , G01S5/00 , G01S5/02 , G01S13/882 , G01S13/9303 , G01S13/94 , G01S15/93 , G01S17/933 , G05D1/12 , G08G5/0069
Abstract: Embodiments described herein may relate to an unmanned aerial vehicle (UAV) navigating to a target in order to provide medical support. An illustrative method involves a UAV (a) determining an approximate target location associated with a target, (b) using a first navigation process to navigate the UAV to the approximate target location, where the first navigation process generates flight-control signals based on the approximate target location, (c) making a determination that the UAV is located at the approximate target location, and (d) in response to the determination that the UAV is located at the approximate target location, using a second navigation process to navigate the UAV to the target, wherein the second navigation process generates flight-control signals based on real-time localization of the target.
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公开(公告)号：US20180244365A1
公开(公告)日：2018-08-30
申请号：US15904149
申请日：2018-02-23
Applicant: Vantage Robotics, LLC
Inventor： Tobin Fisher , Johannes Becker Van Niekerk , Craig Janik
CPC classification number: B64C1/069 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2211/00 , B64D47/08
Abstract: A modular unmanned aerial vehicle (UAV) can include a main body and one or more peripherals configured to be removably attached to the main body. The main body can be configured to identify the peripheral, such as through the provision of an identifying signal on the provisional. The processor can cause the UAV to execute a function based at least in part on the identification of the attached peripheral, or by user interaction with the peripheral or another component of the UAV.
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Patent Agency Ranking
公开(公告)号：US10059444B2
公开(公告)日：2018-08-28
申请号：US14180312
申请日：2014-02-13
Applicant: ARINC Incorporated
Inventor： Rolf Stefani
CPC classification number: B64C39/024 , B64C2201/12 , B64C2201/14 , B64C2201/146 , G05D1/0016 , G08G5/0008 , G08G5/0013 , G08G5/0069 , G08G5/0078 , G08G5/0082
Abstract: A system and method are provided to support accommodating safe integration of small unmanned aircraft systems (sUASs) into the National Airspace Structure in the United States and to augment previously untracked aircraft positions by opportunistically acquiring their position information and forwarding this information to other systems for display. The disclosed schemes integrate automatic dependent surveillance-broadcast (ADS-B) capabilities in sUASs by providing an ADS-B receiver on the small unmanned aircraft or in association with a ground-based sUAS control and communication workstation. Processing of the ADS-B information is integrated with processing of acquired information on sUAS aerial platform operations. Processed integrated information is displayed locally on the workstation and transmitted to other facilities to be remotely displayed. Acquired position information for the sUAS aerial platform and manned aerial vehicles in a vicinity of the sUAS aerial platform are converted to formats commonly used by air traffic control systems.
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公开(公告)号：US10012999B2
公开(公告)日：2018-07-03
申请号：US14991846
申请日：2016-01-08
Applicant: Microsoft Technology Licensing, LLC
Inventor： Ranveer Chandra , Ashish Kapoor , Jongho Won
CPC classification number: G05D1/0808 , B64C27/00 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2201/141 , B64C2201/146 , G05D1/0011 , G05D1/0202 , G05D1/0204 , G05D1/08 , G05D1/0858
Abstract: Methods and apparatus for avoiding or exploiting air drag on an aerial vehicle are disclosed. In embodiments, the methods and apparatus may be implemented in a controller and used to increase the energy efficiency of an aerial vehicle. In the embodiments, at least one parameter associated with a force on an aerial vehicle is determined. A yaw setting for the aerial vehicle is then determined that exploits or avoids air drag on the aerial vehicle for energy efficiency. The yaw setting may be referenced to a yaw based on directionality in the shape of the aerial vehicle. In other embodiments, a drag associated with a force on an aerial vehicle is determined. It is then determined if there is a selected component in the drag based on a desired maneuver of the aerial vehicle. A yaw setting is then determined based on whether the selected component is in the drag.
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公开(公告)号：US10007890B1
公开(公告)日：2018-06-26
申请号：US14752725
申请日：2015-06-26
Applicant: Amazon Technologies, Inc.
Inventor： Oliver Christoph Purwin , Andrew Stubbs
CPC classification number: G06Q10/087 , B64C39/024 , B64C2201/022 , B64C2201/128 , B64C2201/14 , B64C2201/162 , G08G5/0069
Abstract: The disclosed inventory systems and methods can be used to retrieve and transport items from one location in an inventory system to another. Specifically, an unmanned aerial vehicle (UAV) including passive buoyancy element, a thrust unit, and a retention feature, can be controlled by a management component to retrieve one or more items, transport the item or items, and deposit the item or items. For example, a UAV can be controlled to obtain an item at one location in a warehouse such as a first floor and lift said item to a second location in the warehouse such as a second floor, and deposit the item at the second location.
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公开(公告)号：US20180157276A1
公开(公告)日：2018-06-07
申请号：US15829690
申请日：2017-12-01
Applicant: Vantage Robotics, LLC
Inventor： Tobin Fisher , Johannes Becker Van Niekerk , Pavlo Manovi
CPC classification number: G05D1/102 , B64C39/024 , B64C2201/042 , B64C2201/08 , B64C2201/14 , B64C2201/141 , B64D47/02 , G01C21/16 , G01C21/18
Abstract: A unmanned aerial vehicle (UAV) includes a body with plurality of motors, a motor controlling circuit, a microprocessor for controlling the flight state of the UAV, a plurality of motion sensors, and a capacitive touch sensor incorporated into a battery. When the user grasps the UAV by the battery, the touch sensor is activated and the microprocessor alters the flight state of the UAV.
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公开(公告)号：US20180156610A1
公开(公告)日：2018-06-07
申请号：US15870174
申请日：2018-01-12
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor： Zhenyu ZHU , Zihan CHEN , Zhiyuan ZHANG , Weifeng LIU , Chaobin CHEN
IPC: G01C3/08 , G01C9/00 , G05D1/10 , G05D1/00 , G08G5/04 , G06K9/00 , G06K9/20 , G06K9/62 , G06K9/78 , G06T7/60 , G06T7/246 , G06T7/292
CPC classification number: G01C3/08 , B64C2201/14 , G01C3/14 , G01C9/005 , G05D1/0094 , G05D1/10 , G06K9/0063 , G06K9/209 , G06K9/4671 , G06K9/6202 , G06K9/78 , G06K2209/21 , G06T7/248 , G06T7/292 , G06T7/593 , G06T7/60 , G06T2207/10012 , G06T2207/10032 , G06T2207/30261 , G08G5/0021 , G08G5/0069 , G08G5/04 , G08G5/045
Abstract: A method for distance detection includes detecting a first distance value between a movable object and a target object in a target direction of the movable object, obtaining an inclination angle of the movable object at the target direction, and calculating a second distance value from the movable object to the target object based upon the inclination angle and the first distance value.
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