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    IMAGE AND/OR RADIO SIGNALS CAPTURING PLATFORM
    35.
    发明申请
    IMAGE AND/OR RADIO SIGNALS CAPTURING PLATFORM 审中-公开

    公开(公告)号：US20170205536A1

    公开(公告)日：2017-07-20

    申请号：US15326764

    申请日：2015-07-17

    Applicant: ALTEC S.P.A.

    Inventor： Ivano MUSSO

    IPC: G01W1/08 ,  H04N5/232 ,  B63B35/00 ,  H04N5/225 ,  B64D1/12 ,  B64D47/08 ,  G01S13/95 ,  H04N7/18

    CPC classification number: G01W1/08 ,  B63B35/00 ,  B64C2201/022 ,  B64C2201/125 ,  B64C2201/127 ,  B64D1/12 ,  B64D47/08 ,  G01C11/02 ,  G01S13/953 ,  G01S13/956 ,  G03B15/006 ,  G03B17/08 ,  G03B17/561 ,  G05D1/0094 ,  H04N5/2252 ,  H04N5/23238 ,  H04N7/18

    Abstract: Platform (100; 200, 200′, 200″) configured to acquire images and/or radio signals and to be carried by lightweight aviation aircrafts, characterised in that it comprises housing means (1, 3; 22, 201, 202, 203, 31) that houses one or more acquisition sensors selected from the group comprising or consisting of cameras (5; 51; 32) configured to acquire still and/or moving images and radio signal receivers (62; 34) configured to acquire radio signals, said housing means (1, 3; 22, 201, 202, 203, 31) being configured to be coupled to a light aviation aircraft (540), said one or more acquisition sensors (5; 51; 32; 62; 34) being connected to processing means (6; 23) configured to receive sensing data from a position and motion sensing unit (10; 230) coupled to said one or more acquisition sensors (5; 51; 32; 62; 34), said processing means (6; 23) being configured to control and/or program, on the basis of the received sensing data, each acquisition sensor (5; 51; 32; 62; 34) so as to enable the same to acquire images and/or radio signals when such acquisition sensor (5; 51; 32; 62; 34) is in a determined position and is subject to oscillations having a velocity that is not larger in absolute value than a maximum oscillation velocity value, whereby a rate of variation of an actual aiming of such acquisition sensor (5; 51; 32; 62; 34) is not larger in absolute value than a respective maximum value of rate of variation of offset with respect to an ideal aiming at a target, so as to ensure focusing of such acquisition sensor (5; 51; 32; 62; 34) on an aimed area.

    METHOD AND SYSTEM FOR CONFIGURABLE AND SCALABLE UNMANNED AERIAL VEHICLES AND SYSTEMS
    39.
    发明申请
    METHOD AND SYSTEM FOR CONFIGURABLE AND SCALABLE UNMANNED AERIAL VEHICLES AND SYSTEMS 审中-公开
    可配置和可扩展的无人驾驶飞机和系统的方法和系统

    公开(公告)号：US20170021946A1

    公开(公告)日：2017-01-26

    申请号：US15206645

    申请日：2016-07-11

    Applicant: LIMITLESS COMPUTING, INC.

    Inventor： ERRIN T. WELLER ,  JEFFREY B. FRANKLIN

    IPC: B64F5/00 ,  B64D45/00 ,  G05D1/00 ,  B64C39/02 ,  B64D47/08

    CPC classification number: G06K19/0723 ,  B64C39/024 ,  B64C2201/125 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/146 ,  B64D45/00 ,  B64D47/08 ,  B64F5/10 ,  B64F5/60 ,  G06F3/00 ,  G06F3/0482 ,  G06F11/00 ,  G06Q10/00 ,  G06Q50/30 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/0069

    Abstract: An unmanned aircraft system (UAS) making use of unmanned aerial vehicles (UAVs) for more than one task. The inventors discovered that an improved UAS could be provided by combining one or more of these three elements: (1) hot-swappable modular kits (e.g., a plurality of components useful in UAVs to perform particular user-selectable tasks); (2) an interconnection mechanism for each component with identification protocols that provides both a physical and a data connection; and (3) an intelligent system that interprets the identification protocols and determines the configuration for a selected task, error checking, airworthiness, and calibration. The system and associated methods for the task based drone configuration and verification reduces the possibility of task failure by an operator.

    Abstract translation: 无人驾驶飞机系统（UAS）利用无人机（UAV）进行多项任务。 本发明人发现，可以通过组合这三个元件中的一个或多个来提供改进的UAS：（1）热插拔模块化套件（例如，在UAV中可用于执行特定用户可选择的任务的多个组件）; （2）具有提供物理和数据连接的识别协议的每个组件的互连机制; 和（3）智能系统，其解释识别协议并确定所选任务的配置，错误检查，适航性和校准。 用于基于任务的无人机配置和验证的系统和相关方法减少了操作员发生任务故障的可能性。

    SYSTEM AND METHOD FOR PROVIDING ACCURACY IN AIRDROP MISSIONS
    40.
    发明申请
    SYSTEM AND METHOD FOR PROVIDING ACCURACY IN AIRDROP MISSIONS 审中-公开
    在空中任务中提供精度的系统和方法

    公开(公告)号：US20140142788A1

    公开(公告)日：2014-05-22

    申请号：US14040816

    申请日：2013-09-30

    Applicant: UNITED STATES AIR FORCE

    Inventor： ROBERT J. DENTON

    IPC: B64C19/00 ,  G01W1/00

    CPC classification number: G01W1/00 ,  B64C39/024 ,  B64C2201/122 ,  B64C2201/125 ,  B64C2201/128

    Abstract: System and method for aiding the accuracy of airdrop missions by performing localized weather data collection in a column of air and then subsequently storing, decimating and forwarding the data to a remote location. A first aircraft flies to the geographic location of the desired airdrop, deploys an atmospheric conditions sensing dropsonde, collects the data from the dropsonde, stores that data, then transmits that data or a decimated subset of that data either once or any number of consecutive times, to a second aircraft located at a predetermined distance from the first aircraft.

    Abstract translation: 通过在一列空气中执行本地化天气数据，然后将数据存储，抽取和转发到远程位置来辅助空投任务的准确性的系统和方法。 第一架飞机飞往所需空投的地理位置，部署一个大气条件检测水滴探测器，收集数据，然后存储该数据，然后传送该数据或该数据的抽取子集一次或任意数量的连续时间 到位于距离第一飞行器预定距离的第二飞行器。

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