公开(公告)号：US20140152090A1

公开(公告)日：2014-06-05

申请号：US14177147

申请日：2014-02-10

申请人： INSCOPE ENERGY, LLC

发明人： Jason Craig ,  Kevin Cassidy ,  Richard Daniel Albarran

IPC分类号： B60R16/03

CPC分类号： B60R16/033 ,  B60L11/1851 ,  B60R16/03 ,  B63G8/001 ,  B63G2008/002 ,  G05D1/0088 ,  G05D1/10 ,  H02J3/14 ,  H02J4/00 ,  Y10T307/305 ,  Y10T307/391

摘要： The operation and/or power of a plurality of energy loads and/or energy supplies configured to supply power to the energy loads are managed in a coordinated manner. The coordinated control over the energy loads and/or energy supplies may enable the execution of missions including a one or more objectives by energy loads with an enhanced efficiency, autonomy, and/or effectiveness. Aspects of the planning and/or management of execution of the missions may be automated according to predetermined rules and/or criteria.

摘要翻译： 以协调的方式管理被配置为向能量负载供电的多个能量负载和/或能量供应的操作和/或功率。 对能量负载和/或能量供应的协调控制可以使得能够以提高的效率，自主性和/或有效性的能量负载来执行包括一个或多个目标的任务。 可以根据预定的规则和/或标准自动执行规划和/或管理执行任务的方面。

公开(公告)号：US20140081505A1

公开(公告)日：2014-03-20

申请号：US13724414

申请日：2012-12-21

申请人： PROXY TECHNOLOGIES INC.

发明人： John Solomon Klinger ,  Robert F. Davis

IPC分类号： G05D1/10

CPC分类号： G08G9/02 ,  G05D1/0027 ,  G05D1/10 ,  G05D1/104 ,  G08G1/162 ,  G08G1/163 ,  G08G5/0004 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/003 ,  G08G5/0069 ,  G08G5/04 ,  G08G5/045 ,  G08G5/065

摘要： A non-transitory processor-readable medium storing code causes a processor at a first vehicle (e.g., a first autonomous vehicle) to generate a first planned path based on a current position of the first vehicle and a mission requirement assigned to the first vehicle. A first planned path associated with a second vehicle (e.g., a second autonomous vehicle), which is based on a current position of the second vehicle and a mission requirement assigned to the second vehicle, is received at the first vehicle. After the first planned path associated with the second vehicle is received, a second planned path is generated based on the first planned path associated with the second vehicle and at least one of the mission requirement assigned to the first vehicle or the first planned path of the first vehicle. The second planned path of the first vehicle is transmitted to the second vehicle.

摘要翻译： 存储代码的非暂时处理器可读介质使得第一车辆（例如，第一自主车辆）处的处理器基于第一车辆的当前位置和分配给第一车辆的任务要求来生成第一计划路径。 在第一车辆处接收与第二车辆（例如，第二自主车辆）相关联的第一计划路径，其基于第二车辆的当前位置和分配给第二车辆的任务要求。 在接收到与第二车辆相关联的第一计划路径之后，基于与第二车辆相关联的第一计划路径和分配给第一车辆的任务要求或第一车辆的第一计划路径中的至少一个生成第二计划路径 第一辆车。 第一车辆的第二计划路径被发送到第二车辆。

公开(公告)号：US20130138272A1

公开(公告)日：2013-05-30

申请号：US13685880

申请日：2012-11-27

申请人： Airbus Operations SAS

发明人： Pascale Louise-Babando ,  Delphine Macdonald ,  Raphaëlle Ankaoua

IPC分类号： G05D1/10

CPC分类号： G05D1/10 ,  G01C23/00 ,  G06F3/0362 ,  G06F3/04847 ,  G06F3/04883 ,  G06F3/04886

摘要： The dialog device includes a display screen, on which are displayed three graphic representations, which are respectively associated with the three control axes of the aircraft, each of said graphic representations comprising a plurality of portions, each of which is associated with a guidance mode of the associated control axis, so that all the possible guidance modes of the guidance system are thus represented, this representation highlighting the fact that the guidance modes are active exclusively on a given guidance axis.

摘要翻译： 对话装置包括显示屏幕，显示屏幕分别与飞机的三个控制轴相关联，每个所述图形表示包括多个部分，每个部分与引导模式相关联 相关联的控制轴，从而由此表示引导系统的所有可能的引导模式，该表示突出显示引导模式仅在给定引导轴上有效的事实。

公开(公告)号：US07257483B2

公开(公告)日：2007-08-14

申请号：US11376300

申请日：2006-03-16

申请人： Michel Blain ,  Régis Houde ,  Richard Laliberté

发明人： Michel Blain ,  Régis Houde ,  Richard Laliberté

IPC分类号： G01C21/00

CPC分类号： G05D1/10

摘要： A method and apparatus is disclosed for providing a determined position in real-time of an underwater object using a plurality of sensors operating at various sampling rates and for using the determined position in real-time in order to perform inspection tasks inter alia.

公开(公告)号：US06771563B1

公开(公告)日：2004-08-03

申请号：US10239236

申请日：2002-09-20

申请人： François Bernard

发明人： François Bernard

IPC分类号： B63C1142

CPC分类号： B63J99/00 ,  B63C11/42 ,  B63G8/42 ,  B63J2099/008 ,  E21B19/002 ,  E21B41/04 ,  G01S5/0009 ,  G01S5/22 ,  G01S15/74 ,  G01S19/41 ,  G01S19/44 ,  G01S19/47 ,  G05D1/10

摘要： Apparatus (50) for deploying an object to an underwater target position, the apparatus being provided with a beacon to transmit acoustic rays, a plurality of thrusters (56(i), i=1, 2, . . . I, I being an integer) to control positioning of the apparatus with respect to the underwater target position, and a sound velocity meter to measure velocity of sound in a fluid surrounding the apparatus.

摘要翻译： 用于将物体部署到水下目标位置的装置（50），所述装置设置有用于传输声射线的信标，多个推进器（56（i），i = 1,2，...，I， 整数）以控制装置相对于水下目标位置的定位;以及声速计，用于测量装置周围的流体中的声速。

公开(公告)号：US20190243389A1

公开(公告)日：2019-08-08

申请号：US16314681

申请日：2017-06-20

申请人： SHANGHAI HUACE NAVIGATION TECHNOLOGY LTD

发明人： Shengfei DONG ,  Jiejun WANG ,  Caimeng LI ,  Huazhong XIE ,  Wei HE

IPC分类号： G05D1/10 ,  G01S19/41 ,  G01S19/49 ,  B64C39/02 ,  G08G5/00

CPC分类号： G05D1/101 ,  B64C39/024 ,  B64C2201/141 ,  G01S19/41 ,  G01S19/48 ,  G01S19/49 ,  G05D1/10 ,  G08G5/0069

摘要： A flight control system of an unmanned aerial vehicle with differential positioning based on a CORS network includes a MEMS sensing unit for collecting data of angular velocity, linear velocity, air pressure, and magnetic field; a GNSS positioning unit for acquiring GNSS positioning data; a network communication unit for acquiring CORS differential data; an attitude/navigation control unit for controlling the attitude and navigation of the unmanned aerial vehicle, a main control unit for performing data processing, data fusion and system control operations among functional units. The 3G mobile network is used to obtain the differential data from CORS base station and realize an RTK differential positioning of the flight control system, which can satisfy the requirements of centimeter-level positioning accuracy of unmanned aerial vehicles for high-end consumer market and professional surveying and mapping.

公开(公告)号：US20190236966A1

公开(公告)日：2019-08-01

申请号：US15884970

申请日：2018-01-31

申请人： General Electric Company

发明人： Szabolcs BORGYOS ,  Susan ROBERTS ,  Vineet MEHTA ,  John SPIRTOS ,  Ashish JAIN

IPC分类号： G08G9/02 ,  G05D1/00 ,  G08G7/02 ,  G05D1/10

CPC分类号： G08G9/02 ,  G05D1/0044 ,  G05D1/10 ,  G08G7/02

摘要： According to some embodiments, a centralized registry data store may contain electronic records that represent movement plan contracts for Unmanned Vehicles (“UVs”). A centralized registry platform may receive information about a potential movement plan contract for a UV and dynamically create a potential multi-dimensional, time-indexed volume representing the potential movement plan contract. The centralized registry platform may then automatically compare the potential multi-dimensional, time-indexed volume with another volume representing another movement plan contract that was previously registered with the centralized registry platform. Based on a result of the comparison, the centralized registry platform may dynamically register the potential movement plan contract in the centralized registry data store.

公开(公告)号：US20190221128A1

公开(公告)日：2019-07-18

申请号：US16361659

申请日：2019-03-22

申请人： SZ DJI TECHNOLOGY CO., LTD.

发明人： Zhuo GUO ,  Zhuo XIE ,  Zebo YANG ,  Wenlin LI ,  Lei WANG ,  Ding WANG ,  Haoyu LI

IPC分类号： G08G5/04 ,  G08G5/00 ,  B64C39/02 ,  G05D1/00

CPC分类号： G08G5/045 ,  B64C39/024 ,  B64C2201/146 ,  G05D1/0016 ,  G05D1/10 ,  G08G5/0013 ,  G08G5/0039

摘要： A flight control method includes acquiring, by a smart terminal, data of at least two flight routes. The flight control method also includes associating, by the smart terminal and based on preset information of at least two aircrafts, at least one aircraft with a flight route of the at least two flight routes. The flight control method further includes based on a result of the associating, sending, by the smart terminal, data of the flight route to the associated at least one aircraft.

公开(公告)号：US20180326441A1

公开(公告)日：2018-11-15

申请号：US15774804

申请日：2016-11-04

申请人： Xiaoyang LIU ,  Haiying LIN

发明人： Xiaoyang LIU ,  Haiying LIN

IPC分类号： B05B13/00 ,  G05D1/10 ,  B05B15/62 ,  B05B1/20 ,  G05D1/00 ,  B64C39/02 ,  G05D1/04

CPC分类号： B05B13/005 ,  B05B1/20 ,  B05B15/62 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/12 ,  B64C2201/148 ,  G05D1/0027 ,  G05D1/042 ,  G05D1/10 ,  G05D1/104

摘要： A tethered unmanned rotorcraft chain platform system and liquid continuous spraying system includes a mobile mooring platform, a power system, a tether, multiple unmanned rotorcrafts, a central control system and a liquid continuous spraying system. The power system moves with the mobile mooring platform and provides electrical power to the multiple unmanned rotorcrafts by the tether. The tether is lifted in the air by the multiple unmanned rotorcrafts to form a three-dimensional polyline/curve, so as to avoid or bypass obstacles and adapt to the terrain variation, thus greatly expanding the horizontal space that can be reached by the tethered unmanned rotorcraft chain and its payload. The delivery pipeline of the liquid continuous spraying system is arranged along the tether to continuously supply a liquid such as agricultural chemicals to spraying nozzles mounted on the delivery pipeline or the unmanned rotorcrafts.

公开(公告)号：US10036716B2

公开(公告)日：2018-07-31

申请号：US15305063

申请日：2014-04-22

申请人： SKYROBOT INC.

发明人： Ryohei Uetaki ,  Daisuke Kaio

IPC分类号： H04N7/18 ,  G01N25/72 ,  G01J5/00 ,  G01J5/04 ,  H04N5/33 ,  G06K9/00 ,  B64C39/02 ,  B64D47/08 ,  B64D17/80 ,  B64D45/00 ,  G05D1/10 ,  H02S50/10

CPC分类号： G01N25/72 ,  B64C39/024 ,  B64C2201/146 ,  B64D17/80 ,  B64D45/00 ,  B64D47/08 ,  B64D2201/00 ,  G01J5/0066 ,  G01J5/047 ,  G01J5/089 ,  G01J5/10 ,  G01J2005/0077 ,  G01J2005/0081 ,  G05D1/10 ,  G06K9/0063 ,  H02S50/10 ,  H04N5/33

摘要： A solar power panel failure search and detect system to search and detect malfunctioning or failed sites of a solar power panel. A search unit is installed in a remotely controllable aerial vehicle. The search unit maintains a constant distance between a solar panel and a failure detector, and maintains the failure detector at an optimum angle. A control unit controls a flight path and a flight angle of the aerial vehicle and controls/regulates an angle of the failure detector, a receiver, a processor, and the search unit. The search unit has an angle sensor, the failure detector, an angle adjuster and an imaging device. The control unit has a transmitter to transmit the search result data.