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    基于最小树形图的无人机编队通信拓扑重优化方法及系统
    11.
    发明授权
    基于最小树形图的无人机编队通信拓扑重优化方法及系统 有权

    公开(公告)号：CN105873171B

    公开(公告)日：2017-05-03

    申请号：CN201610383787.3

    申请日：2016-05-27

    Applicant: 合肥工业大学

    Inventor： 罗贺 ,  王国强 ,  胡笑旋 ,  马华伟 ,  靳鹏 ,  夏维

    IPC: H04W40/24

    CPC classification number: H04W28/021 ,  B64C39/024 ,  B64C2201/143 ,  G08G5/0008 ,  G08G5/0052 ,  G08G5/0069 ,  G08G5/045 ,  H04W40/00 ,  H04W84/18

    Abstract: 本发明提供了一种基于最小树形图的无人机编队通信拓扑重优化方法及系统，用于在编队中的无人机出现通信故障后，对重构后的无人机编队通信拓扑的优化，该方法包括：计算重构后的无人机编队通信拓扑的第一通信代价；将所述第一通信代价与预设状态下的编队通信图的最小树形图的目标通信代价进行比较；在第一通信代价大于目标通信代价时，通过预设策略优化所述重构后的无人机编队通信拓扑。本发明通过将重构后的无人机编队通信拓扑的第一通信代价，与目标通信代价进行比较，在第一通信代价大于目标通信代价时，通过预设策略优化所述重构后的无人机编队通信拓扑，使得编队中的无人机出现通信故障时，重优化后的无人机编队通信拓扑的通信代价最小。

    METHODS AND APPARATUS TO COOPERATIVELY LIFT A PAYLOAD
    16.
    发明授权
    METHODS AND APPARATUS TO COOPERATIVELY LIFT A PAYLOAD 有权

    公开(公告)号：EP3210886B1

    公开(公告)日：2018-12-12

    申请号：EP17165314.0

    申请日：2014-09-18

    Applicant: The Boeing Company

    Inventor： Jones, Richard Donovan ,  Duffy, Michael J.

    IPC: B64C39/02 ,  B64D1/22 ,  G05D1/08 ,  G05D1/10

    CPC classification number: B64C19/02 ,  B64C39/024 ,  B64C2201/128 ,  B64C2201/143 ,  B64C2201/145 ,  B64D1/22 ,  G05D1/0858 ,  G05D1/104

    Abstract: Methods and apparatus to cooperatively lift a payload (110) are disclosed. An example method to control a lift vehicle (102) includes determining (704) a first positional state of the lift vehicle (102) with respect to a payload (110) controlled by a plurality of lift vehicles (102, 104, ...) including the lift vehicle (102), determining (706) a second positional state of the lift vehicle (102) with respect to a goal location, detecting distances (708) to the other ones of the plurality of lift vehicles (102, 104, ...), determining (710) a third positional state of the lift vehicle (102) based on the distances to the other ones of the plurality of lift vehicles (102, 104, ...), and calculating (712-720) a control command to control the lift vehicle (102) based on the first positional state, the second positional state, and the third positional state.

    COMBINATION OF UNMANNED AERIAL VEHICLES AND THE METHOD AND SYSTEM TO ENGAGE IN MULTIPLE APPLICATIONS
    17.
    发明公开
    COMBINATION OF UNMANNED AERIAL VEHICLES AND THE METHOD AND SYSTEM TO ENGAGE IN MULTIPLE APPLICATIONS 有权
    KOMBINATION AUS UNBEMANNTEN LUFTFAHRZEUGEN SOWIE VERFAHREN UND SYSTEM ZUM EINSATZ IN MEHREREN ANWENDUNGEN

    公开(公告)号：EP3055208A4

    公开(公告)日：2017-05-31

    申请号：EP13895435

    申请日：2013-11-08

    Applicant: DE SILVA SHELTON GAMINI

    Inventor： DE SILVA SHELTON GAMINI

    IPC: B64C39/02 ,  B64D5/00 ,  G05D1/00

    CPC classification number: B64D5/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/082 ,  B64C2201/122 ,  B64C2201/126 ,  B64C2201/143 ,  B64C2201/145 ,  B64C2201/206 ,  B64D47/08 ,  G05D1/0011 ,  G05D1/104

    Abstract: This invention relates to an Unmanned Aerial Vehicle hereinafter called “Mother UAV” member (11) capable of carrying modules of Sub Unmanned Aerial Vehicle members (12) hereinafter called “Sub UAV” member. More particularly, the method and system that is capable of communicating via satellite and remote control technology wherein ejecting said Sub UAV members (12) from the Mother UAV member (11) wherein Sub UAV members (12) autonomously fly in sequence in a coordinated manner with the Mother UAV member (11), and capable of engaging in multiple missions in high, medium, low altitude, and surface, also communication with under sea submarines (27). Further, comprises of a method and system that the Sub UAV members (12) are able to return back to the Mother UAV member (11) after the mission is completed and be firmly secured to the flatbed (14) of the Mother UAV member (11). The present invention is specifically designed for multifunctional and multipurpose applications where humans and other vehicles are unable to access, for civil, commercial and military purposes.

    Abstract translation: 本发明涉及一种能够承载以下称为“Sub UAV”成员的子无人驾驶飞机构件（12）的模块的以下称为“母亲UAV”构件（11）的无人驾驶飞行器（11）。 更具体地说，能够通过卫星和远程控制技术进行通信的方法和系统，其中从UAV无人机构件（11）中弹出所述无人驾驶飞行器构件（12），其中无人机UAV构件（12）以协调的方式 与母亲无人机成员（11），并能够在高，中，低海拔和水面进行多项任务，并且还可以与海底潜艇进行通信（27）。 此外，包括一种方法和系统，使得在完成任务后Sub UAV部件（12）能够返回到母机（11）并牢固地固定到母UAV部件（11）的平板（14） 11）。 本发明特别设计用于人和其他车辆无法进入的用于民用，商业和军事目的的多功能和多用途应用。

    MODULAR ARTICULATED-WING AIRCRAFT
    18.
    发明公开
    MODULAR ARTICULATED-WING AIRCRAFT 有权
    带翅膀的链接模块化飞机

    公开(公告)号：EP1924495A2

    公开(公告)日：2008-05-28

    申请号：EP06851409.0

    申请日：2006-06-28

    Applicant: Sommer, Geoffrey S.

    Inventor： Sommer, Geoffrey S.

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C37/02 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/143 ,  B64C2201/165 ,  B64C2201/206

    Abstract: Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and/or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.

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