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公开(公告)号:US10009518B2
公开(公告)日:2018-06-26
申请号:US14971506
申请日:2015-12-16
Applicant: INDUSTRIAL TECHNOLOGY RESEARCH INSTITUTE
Inventor: Wei-Ying Tai , Chan-Ru Chang , Chun-Wen Tang
CPC classification number: H04N5/2252 , B64C39/028 , B64C2201/027 , B64C2201/042 , B64C2201/127 , B64C2201/201 , H04N5/2251
Abstract: A detachable aerial photographic apparatus includes a carrier, an aircraft, a take-off delaying device and a trigger. The aircraft includes a main body disposed on the carrier, at least one propeller is pivotally furnished in the main body and a camera disposed on the main body. The take-off delaying device includes a movable member disposed on the carrier and at least one stopper connected to the movable member. The stopper is detachably connected to the aircraft for prevent the aircraft from taking off. The movable member is for detaching the stopper from the aircraft for releasing the aircraft. The trigger is electrically connected to the aircraft and the take-off delaying device. The trigger is for triggering the propeller and the movable member. A first time point when the propeller is triggered by the trigger is earlier than a second time point when the stopper is detached from the aircraft.
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公开(公告)号:US10008123B2
公开(公告)日:2018-06-26
申请号:US15659133
申请日:2017-07-25
Applicant: Skycatch, Inc.
Inventor: David Chen
CPC classification number: G08G5/0034 , B64C39/024 , B64C2201/123 , B64C2201/127 , B64C2201/141 , G01C11/00 , G05D1/0094 , G05D1/0202 , G08G5/006 , G08G5/0069 , G08G5/0086
Abstract: Systems and methods are disclosed for generating a digital flight path within complex mission boundaries. In particular, in one or more embodiments, systems and methods generate flight legs that traverse a target site within mission boundaries. Moreover, one or more embodiments include systems and methods that utilize linking algorithms to connect the generated flight legs into a flight path. Moreover, one or more embodiments include systems and methods that generate a mission plan based on the flight path. In one or more embodiments, the generated mission plan enables a UAV to traverse a flight area within mission boundaries and capture aerial images with regard to the target site. Furthermore, in one or more embodiments, systems and methods capture digital aerial images of vertical surfaces of a structure by generating a reference surface and flight legs corresponding to the reference surface.
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公开(公告)号:US10000284B1
公开(公告)日:2018-06-19
申请号:US14752746
申请日:2015-06-26
Applicant: Amazon Technologies, Inc.
Inventor: Oliver Christoph Purwin , Andrew Stubbs
CPC classification number: B64C39/024 , B64B1/26 , B64B1/40 , B64C2201/022 , B64C2201/127 , B64C2201/128 , B64C2201/148 , B64C2201/162 , B64C2201/182
Abstract: The disclosed unmanned aerial vehicle (UAV) includes a buoyant airbag, a drive unit, a retention feature, and an onboard control module that can be configured to cause the drive unit to displace the UAV, cause the retention feature to retain one or more items for transport, and receive instructions to transfer items from one location to another. For example, a UAV can be controlled to obtain an item at one location in a warehouse such as a first floor, 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:US09998669B2
公开(公告)日:2018-06-12
申请号:US15341440
申请日:2016-11-02
Applicant: Samsung Electronics Co., Ltd.
Inventor: Yoon-Seok Kang , Sungjin Park , Baeseok Lim
CPC classification number: H04N5/23287 , B64C39/024 , B64C2201/127 , B64D47/08 , F16M11/123 , G03B15/006 , G03B17/561 , H04N5/2253 , H04N5/2254
Abstract: A camera gimbal is provided. The camera gimbal includes a gimbal barrel; a lens barrel configured to support a camera module thereon, and assembled to the gimbal barrel; and a connection unit configured to interconnect the gimbal barrel and the lens barrel, wherein the lens barrel is connected to be freely rotatable, wherein the connection unit provides a rolling axis, a yawing axis, and a pitching axis of the lens barrel, and wherein the lens barrel assembled to the connection unit is configured to maintain a horizontal posture by gravity.
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公开(公告)号:US09994316B1
公开(公告)日:2018-06-12
申请号:US15381601
申请日:2016-12-16
Applicant: Amazon Technologies, Inc.
Inventor: Amir Navot , Scott Raymond Harris , Daniel Buchmueller
CPC classification number: B64C39/024 , B64C39/02 , B64C2201/024 , B64C2201/027 , B64C2201/127 , B64C2201/141 , B64C2201/145 , B64D45/00 , B64D2045/0085 , G01C21/005 , G01C23/00 , G05D1/0088 , G05D1/0202 , G05D1/0808 , H04L67/12
Abstract: Described are methods and apparatuses for synchronizing two or more sensors of an UAV. In the implementations described, a synchronization event is performed such that identifiable signals of the synchronization event can be collected by each sensor of the UAV. The synchronization event may be generated by a synchronization event component that generates multiple output signals (e.g., audio, visual, and physical) at approximately the same time so that different sensors can each collect and store at least one of the output signals. The collected signals are then compared and the sensors are adjusted to align the signals.
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公开(公告)号:US20180157259A1
公开(公告)日:2018-06-07
申请号:US15868193
申请日:2018-01-11
Applicant: Lucas J. Myslinski
Inventor: Lucas J. Myslinski
CPC classification number: G05D1/0088 , B64C39/024 , B64C2201/126 , B64C2201/127 , B64C2201/141 , B64C2201/22 , B64D5/00 , B64D47/02 , B64D47/08 , G05D1/0094 , G05D1/104 , G06F17/2705 , G06F17/2785 , G06K9/00362 , G06K9/0063 , G06K9/00711 , G06K9/00771 , G06K9/6202 , G06Q10/04 , G06Q10/06 , G06Q10/063 , G06Q10/0833 , G06Q30/0201 , G06Q30/0202 , G06Q30/0207 , G06Q30/0282 , G06Q50/01 , G06Q50/26 , G06T7/20 , G06T2207/10016 , G06T2207/10032 , G06T2207/30196 , G06T2207/30232 , G08B21/18 , H04N5/77 , H04N5/772 , H04N7/183 , H04N7/188
Abstract: A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the information by comparing the information with source information. The social networking fact checking system automatically monitors information, processes the information, fact checks the information and/or provides a status of the information, including automatically modifying a web page to include the fact check results. The fact checking system is able to be implemented utilizing a drone device. The drone device is able to be implemented in conjunction with a security system.
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公开(公告)号:US20180155009A1
公开(公告)日:2018-06-07
申请号:US15833385
申请日:2017-12-06
Applicant: ETH Zurich
Inventor: Mark W. MUELLER , Sergei LUPASHIN , Raffaello D'ANDREA , Markus WAIBEL
CPC classification number: B64C13/24 , B64C27/08 , B64C27/20 , B64C27/32 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2203/00 , B64D45/00 , G05D1/0072
Abstract: 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.
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公开(公告)号:US09989965B2
公开(公告)日:2018-06-05
申请号:US14831739
申请日:2015-08-20
Applicant: Motionloft, Inc.
Inventor: Mark Cuban , Joyce Reitman , Jeffrey Orion Pritchard
CPC classification number: G05D1/0202 , B64C39/024 , B64C2201/123 , B64C2201/127 , B64D47/08 , G05D1/104 , G06K9/0063 , G06K9/00778 , G06K9/52 , H04N5/232 , H04N7/181 , H04N7/185
Abstract: An unmanned aerial vehicle (UAV) can include one or more cameras for capturing image data within a field of view that depends in part upon the location and orientation of the UAV. At least a portion of the image data can be processed on the UAV to locate objects of interest, such as people or cars, and use that information to determine where to fly the drone in order to capture higher quality image data of those or other such objects. Once identified, the objects of interest can be counted, and the density, movement, location, and behavior of those objects identified. This can help to determine occurrences such as traffic congestion or unusual patterns of pedestrian movement, as well as to locate persons, fires, or other such objects. The data can also be analyzed by a remote system or service that has additional resources to provide more accurate results.
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公开(公告)号:US09988145B2
公开(公告)日:2018-06-05
申请号:US15356874
申请日:2016-11-21
Inventor: Wei-Yong Yu
IPC: F16M13/00 , B64C27/00 , B64C39/02 , B64D47/08 , F16M13/02 , F16M11/10 , F16M11/18 , F16M11/20 , G03B15/00
CPC classification number: B64C27/001 , B64C39/024 , B64C2027/002 , B64C2201/027 , B64C2201/127 , B64D47/08 , F16M11/10 , F16M11/18 , F16M11/2071 , F16M13/00 , F16M13/02 , G03B15/006
Abstract: Disclosed is a supporting assembly and an unmanned aerial vehicle using the same, the supporting assembly includes a first base, a second base, a plurality of arms, and a damping element disposed between the first base and the second base. The second base is disposed on the first base. Each of the plurality of arms includes a proximal end and a distal end opposite to the proximal end, the proximal end is secured to the first base, and the distal end is configured for mounting a vibration source.
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公开(公告)号:US09981741B2
公开(公告)日:2018-05-29
申请号:US14858973
申请日:2015-09-18
Applicant: QUALCOMM Incorporated
Inventor: Donald Bolden Hutson
CPC classification number: B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/127
Abstract: Systems and methods are described herein related to an unmanned aerial vehicle, the unmanned aerial vehicle includes: a frame portion, two rear arms extending away from the frame portion, and at least one rear air propulsion device arranged on each of the rear arms at an orthogonal angle relative to a vertical axis. The at least one rear air propulsion device has an axis of rotation for both lift and rotation based on the angle. The unmanned aerial vehicle has two front arms arranged along a horizontal axis. The vertical axis is perpendicular to the horizontal axis. The unmanned aerial vehicle also includes at least one camera arranged on at least one of the front arms. The at least one camera faces a front direction.
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