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    HARDWARE -BASED WEIGHT AND RANGE LIMITATION APPARATUS AND METHOD
    321.
    发明申请
    HARDWARE -BASED WEIGHT AND RANGE LIMITATION APPARATUS AND METHOD 审中-公开
    硬件重量和范围限制装置和方法

    公开(公告)号：WO2013103403A3

    公开(公告)日：2013-09-06

    申请号：PCT/US2012058323

    申请日：2012-10-01

    Applicant: AURORA FLIGHT SCIENCES CORP

    Inventor： WASHINGTON TOM ,  HISAM THORSTEN ,  GOMEZ MARTIN

    IPC: G06F17/00 ,  G05D1/00

    CPC classification number: B64C13/18 ,  B64C2201/145 ,  B64D45/00 ,  G05D1/0055 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/006

    Abstract: The present disclosure endeavors to provide systems, methods and apparatus for ensuring aircraft compliance with governmental guidelines, such as, for example, MRCR Category II compliance. A hardware-based system may be employed to reduce range and/or payload below predetermined ranges and a payload capacities. Also provided herein are hardware-based systems, methods, and apparatus for restricting a system's range to predetermined range and/or the payload to a predetermined limit using, for example, a Application-Specific Integrated Circuit (ASIC) installed in the flight control system.

    Abstract translation: 本公开努力提供用于确保飞机遵守政府准则的系统，方法和装置，例如MRCR II类合规。 可以采用基于硬件的系统来减小低于预定范围和有效载荷容量的范围和/或有效载荷。 本文还提供了基于硬件的系统，方法和装置，其使用例如安装在飞行控制系统中的专用集成电路（ASIC）将系统的范围限制到预定范围和/或有效负载到预定极限 。

    MODULAR FLIGHT MANAGEMENT SYSTEM INCORPORATING AN AUTOPILOT
    322.
    发明申请
    MODULAR FLIGHT MANAGEMENT SYSTEM INCORPORATING AN AUTOPILOT 审中-公开
    包含自动驾驶仪的模块化飞行管理系统

    公开(公告)号：WO2013055441A3

    公开(公告)日：2013-08-01

    申请号：PCT/US2012051227

    申请日：2012-08-16

    Applicant: UNMANNED INNOVATION INC

    Inventor： DOWNEY JONATHAN ,  MICHINI BERNARD

    IPC: G05D1/10

    CPC classification number: G05D1/0088 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/145 ,  G05D1/0055 ,  G05D1/0077 ,  G05D1/0094 ,  G05D1/08 ,  G05D1/101 ,  G06F21/44 ,  H05K3/32 ,  Y10T29/4913

    Abstract: A modular vehicle management system is described, comprising a controller module configured to control different types of carrier modules. The controller module includes a computer system and optionally one or more sensors. The computer system is configured to perform operations comprising detecting whether a carrier module is connected to the controller module. If the carrier module is connected to the controller module, the carrier module is authenticated. If the authentication fails, operation of the vehicle is inhibited. The control module is configured to determine carrier module capabilities including information regarding a navigation processing device, and/or a radio modem. The controller adapts to the capabilities of the controller module. Using information from the sensors and the navigation processing device, the vehicle management system navigates the vehicle.

    Abstract translation: 描述了模块化车辆管理系统，其包括控制器模块，该控制器模块被配置为控制不同类型的载体模块 控制器模块包括计算机系统和可选的一个或多个传感器。 计算机系统被配置为执行包括检测载体模块是否连接到控制器模块的操作。 如果载波模块连接到控制器模块，则载波模块将被认证。 如果认证失败，则车辆的操作被禁止。 控制模块被配置为确定载波模块能力，包括关于导航处理设备和/或无线电调制解调器的信息。 控制器适应控制器模块的功能。 使用来自传感器和导航处理装置的信息，车辆管理系统导航车辆。

    AIRCRAFT LANDING METHOD, SYSTEM AND DEVICE
    323.
    发明申请
    AIRCRAFT LANDING METHOD, SYSTEM AND DEVICE 审中-公开
    飞机着陆方法，系统和装置

    公开(公告)号：WO2007086055A1

    公开(公告)日：2007-08-02

    申请号：PCT/IL2007/000090

    申请日：2007-01-25

    Applicant: ISRAEL AEROSPACE INDUSTRIES LTD. ,  SOMECH, Haim

    Inventor： SOMECH, Haim

    IPC: B64C39/02 ,  B63B35/52 ,  B64D17/80 ,  B64F1/02

    CPC classification number: B64C39/024 ,  B63B35/52 ,  B64C2201/021 ,  B64C2201/084 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/127 ,  B64C2201/145 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/185 ,  B64C2201/205 ,  B64F1/02

    Abstract: The invention provides a system, method and landing device for landing an aircraft (50) with respect to a predetermined landing location (P). The aircraft is configured for powered flight at least when the parafoil (60) is deployed, and includes an automatic landing system for controllably executing a landing approach maneuver for the aircraft while in free powered flight with the parafoil deployed to enable the aircraft to be brought into overlying proximity with the landing location. A landing device in the form of an energy absorbing landing net arrangement (20) is provided at the landing location for enabling the aircraft to be landed thereon at least partially vertically when in overlying proximity, and for dampening the landing impact of the aircraft.

    Abstract translation: 本发明提供了一种用于相对于预定着陆位置（P）降落飞机（50）的系统，方法和着陆装置。 该飞机至少在翼展（60）部署时配置为动力飞行，并且包括一个自动着陆系统，用于在自由动力飞行中可控制地执行飞机的着陆进场操纵，其中部署了翼型飞机以使飞机能够被带到 与着陆位置相邻。 在着陆位置处设置能量吸收着陆网装置（20）形式的着陆装置，用于使飞机在覆盖在邻近位置时至少部分垂直地落在其上，并用于减轻飞机的着陆冲击。

    AIR-LAUNCHABLE AIRCRAFT AND METHOD OF USE
    324.
    发明申请
    AIR-LAUNCHABLE AIRCRAFT AND METHOD OF USE 审中-公开
    可升级的飞机及其使用方法

    公开(公告)号：WO2006036183A1

    公开(公告)日：2006-04-06

    申请号：PCT/US2005/004474

    申请日：2005-02-14

    Applicant: RAYTHEON COMPANY ,  CORDER, David, A. ,  KOESSLER, Jeffrey, H. ,  WEBB, George, R.

    Inventor： CORDER, David, A. ,  KOESSLER, Jeffrey, H. ,  WEBB, George, R.

    IPC: B64C39/02

    CPC classification number: B64C3/56 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/165 ,  B64C2201/201

    Abstract: An air-launched aircraft (10) includes deployable wings (16, 18), elevons (20, 22), and vertical fins (26, 28) that deploy from a fuselage (12) during flight. The aircraft may include a control system for operating the elevons, a communication system, and batteries for powering the systems. In addition, the aircraft may include a payload module (14) that mates with an interface in the fuselage. The payload module may include any of a variety of payloads, including cameras, sensors, and/or radar emitters. The aircraft may be powered or unpowered, and may be very small, for example, less than on the order of 10 kg (22 pounds). The deployable surfaces of the aircraft may be configured to deploy in a pre-determined order, allowing the aircraft automatically to enter controlled flight after being launched in a tumbling mode.

    Abstract translation: 空中飞行器（10）包括在飞行期间从机身（12）展开的可展开的机翼（16,18），电梯（20,22）和垂直翼片（26,28）。 飞机可以包括用于操作电梯的控制系统，通信系统和用于为系统供电的电池。 此外，飞行器可以包括与机身中的接口相配合的有效载荷模块（14）。 有效载荷模块可以包括各种有效载荷中的任何一种，包括相机，传感器和/或雷达发射器。 该飞机可能是动力或无动力的，并且可能非常小，例如小于10kg（22磅）的量级。 飞机的可部署表面可以被配置成以预定的顺序部署，允许飞机在以翻滚模式发射之后自动进入受控飞行。

    ANALYTIC SYSTEM AND ANALYTIC METHOD
    328.
    发明申请
    ANALYTIC SYSTEM AND ANALYTIC METHOD 审中-公开

    公开(公告)号：US20190104496A1

    公开(公告)日：2019-04-04

    申请号：US15574875

    申请日：2017-05-08

    Applicant: Adinte, INC.

    Inventor： Shinji Sogo ,  Kunio Arakawa ,  Manabu Inamori ,  Shingo Fujino

    IPC: H04W64/00 ,  B64C39/02 ,  H04W4/80 ,  H04W4/029 ,  H04B17/318 ,  G05D1/10

    CPC classification number: H04W64/006 ,  B64C39/024 ,  B64C2201/122 ,  B64C2201/145 ,  G01C21/165 ,  G01C21/20 ,  G01C21/26 ,  G05D1/104 ,  G06Q30/02 ,  H04B17/26 ,  H04B17/27 ,  H04B17/318 ,  H04W4/02 ,  H04W4/029 ,  H04W4/80 ,  H04W4/90

    Abstract: The flight control part 201 makes the unmanned aerial vehicle fly along a flight path in a predetermined area. The radio wave acquisition part 202 acquires radio wave information including a radio wave intensity when the radio unit of the unmanned aerial vehicle detects a short-distance radio wave of the user terminal during the flight of the unmanned aerial vehicle. The flight position acquisition part 203 acquires GPS position information of the unmanned aerial vehicle when the radio unit detected the short-distance radio wave, as a flight position of the unmanned aerial vehicle based on a GPS unit of the unmanned aerial vehicle. The terminal position calculation part 204 calculates a presence position of the user terminal in the area based on a radio wave intensity of the acquired radio wave information, and the acquired flight position of the unmanned aerial vehicle. The user attribute analysis part 205 arranges the calculated presence position of the user terminal in the map information corresponding to the area, and analyzes user attribute information of the user terminal based on place attribute information indicating a characteristic of the place where the presence position is arranged.

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