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1. 发明专利

JP2019003693A 航空機認識表示审中-公开
公开(公告)号：JP2019003693A
公开(公告)日：2019-01-10
申请号：JP2018181841
申请日：2018-09-27
申请人： INSITU INC A SUBSIDIARY OF THE BOEING COMPANY
发明人： ANDREW HAYES
IPC分类号： G08G5/00 , B64C13/20 , B64C39/02 , B64F1/36 , G01C21/00 , G09B29/00
摘要：【課題】航空機に関する情報を表示する方法を開示する。【解決手段】地図の第1の部分を示す情報が表示される。当該航空機の現在の高度および当該地図内の地形の間の距離は第1の閾値内にある。地図の第2の部分を示す情報が表示される。当該航空機の当該現在の高度と当該地図内の地形との間の距離が第2の閾値内にある。第1の部分と第2の部分は、当該航空機の当該現在の高度の変化に基づいて更新される。別の例では、航空機の投影された飛行経路を含む地図が表示される。当該航空機および少なくとも一つの地上無線の間の無線周波数(RF)ステータスに関する位置ベースの情報が当該地図に表示される。RFステータスに関する位置ベースの情報が当該航空機の現在位置の変化に基づいて更新される。【選択図】図4

2. 发明公开

KR20180070465A 따르기 위해 운송수단에 대한 타킷에 인접하는 비행 패턴을 수립하기 위한 시스템 및 방법 审中-公开
公开(公告)号：KR20180070465A
公开(公告)日：2018-06-26
申请号：KR20170159594
申请日：2017-11-27
申请人： INSITU INC
发明人： ROLF RYSDYK
IPC分类号： G08G5/00
CPC分类号： G08G5/0034 , B64C39/024 , B64C2201/127 , B64C2201/146 , G03B15/006 , G05D1/0011 , G05D1/0094 , G05D1/101 , G08G5/0013 , G08G5/0039 , G08G5/006
摘要： 따르기위해운송수단에대한타킷에인접하는비행패턴을수립하는예시적방법은타킷에대한원격거리를결정하는단계를포함한다. 원격거리는비행패턴을따른지점에서타킷으로부터의거리를나타낸다. 예시적방법은또한원격거리를기초로렘니스케이트의콘코이달변환의형태로비행패턴을발생시키는단계를포함한다.

3. 发明申请

WO2018111924A1 AERIAL LAUNCH AND/OR RECOVERY FOR UNMANNED AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS 审中-公开
公开(公告)号：WO2018111924A1
公开(公告)日：2018-06-21
申请号：PCT/US2017/065890
申请日：2017-12-12
申请人： INSITU, INC.
发明人： MCGREW, James, Statelar , GRUBB, Matthew, David , DICKSON, Andrew, Keith , HAYES, Andrew, Royds
IPC分类号： B64C39/02 , B64C25/08 , B64C25/10 , B64C25/68 , B64C37/00 , B64C37/02
摘要： Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods. A representative system includes a first, carrier aircraft having an airframe a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover, and a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft. The capture line is sized to releasably engage with a capture device of a second, carried aircraft. The system further includes a retrieval device positioned to support the carried aircraft for detachment from the capture line..

4. 发明申请

WO2014171987A3 AUGMENTED VIDEO SYSTEM PROVIDING ENHANCED SITUATIONAL AWARENESS 审中-公开
标题翻译：增强的视频系统提供增强的状态意识
公开(公告)号：WO2014171987A3
公开(公告)日：2015-09-24
申请号：PCT/US2014013497
申请日：2014-01-29
申请人： INSITU INC
发明人： DAVIDSON DARCY JR , TROWBRIDGE THEODORE T
IPC分类号： G06T19/00 , G05D1/00
CPC分类号： H04N7/183 , G01C11/00 , G01C11/02 , G01C2011/36 , G05D1/0038 , G06T11/00 , G06T11/60 , G06T17/05 , G06T19/006
摘要： A facility, comprising systems and methods, for providing enhanced situational awareness to captured image data is disclosed. The disclosed techniques are used in conjunction with image data, such as a real-time or near real-time image stream captured by a camera attached to an unmanned system, previously captured image data, rendered image data, etc. The facility enhances situational awareness by projecting overlays onto captured video data or "wrapping" captured image data with previously-captured and/or "synthetic world" information, such as satellite images, computer-generated images, wire models, textured surfaces, and so on. The facility also provides enhanced zoom techniques that allow a user to quickly zoom in on an object or area of interest using a combined optical and digital zoom technique. Additionally, the facility provides a digital lead indicator designed to reduce operator-induced oscillations in commanding an image capturing device.
摘要翻译：公开了一种包括系统和方法的设施，用于提供对拍摄图像数据的增强的情境感知。所公开的技术结合图像数据使用，例如由附接到无人系统的相机捕获的实时或接近实时图像流，先前捕获的图像数据，渲染图像数据等。该设施增强了情境感知通过将覆盖物投射到捕获的视频数据上或者使用先前捕获的和/或“合成世界”信息（例如卫星图像，计算机生成的图像，线模型，纹理表面等）“包裹”捕获的图像数据。该设施还提供增强的缩放技术，允许用户使用组合的光学和数字缩放技术快速放大感兴趣的对象或区域。此外，该设施提供了一种数字导联指示器，其设计用于减少操作者引起的命令图像捕获装置的振荡。

5. 发明申请

WO2015073103A3 UNMANNED VEHICLE SEARCHES 审中-公开
标题翻译：未经规定的车辆搜索
公开(公告)号：WO2015073103A3
公开(公告)日：2015-07-02
申请号：PCT/US2014053365
申请日：2014-08-29
申请人： INSITU INC A SUBSIDIARY OF THE BOEING COMPANY , UNIV WASHINGTON
发明人： ARBEIT AMY C , LUM CHRISTOPHER W
IPC分类号： G01C23/00 , G01C21/20 , G08G5/00
CPC分类号： G08G5/0069 , B64C39/024 , B64C2201/127 , B64C2201/14 , G01C21/20 , G01C23/00 , G05D1/0094 , G05D1/0202 , G08G5/0013 , G08G5/0021 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/006
摘要： A method of planning a flight path for a search can include receiving, by a control system, an indication of a search area boundary; receiving, by the control system, an indication of a selected search pattern; determining, by the control system, a flight path based on the search area boundary and the selected search pattern; and transmitting one or more indications of the flight path to an unmanned aerial vehicle.
摘要翻译：规划用于搜索的飞行路径的方法可以包括通过控制系统接收搜索区域边界的指示; 由所述控制系统接收所选择的搜索模式的指示; 通过控制系统确定基于搜索区域边界和所选择的搜索模式的飞行路径; 并将飞行路径的一个或多个指示传送到无人驾驶飞行器。

6. 发明申请

WO2015031281A1 AERIAL VEHICLE TERRAIN AWARENESS DISPLAY 审中-公开
标题翻译： AERIAL车辆TERRAIN意识显示
公开(公告)号：WO2015031281A1
公开(公告)日：2015-03-05
申请号：PCT/US2014/052571
申请日：2014-08-25
申请人： INSITU, INC.(A SUBSIDIARY OF THE BOEING COMPANY)
发明人： HAYES, Andrew
IPC分类号： G08G5/00
CPC分类号： G08G5/0086 , B64C2201/146 , G08G5/0026 , G08G5/0069
摘要： A method of displaying information pertaining to an air vehicle is disclosed. Information is displayed indicative of first portions of a map where distance between a current altitude of the air vehicle and terrain in the map are within a first threshold. Information is displayed indicative of second portions of a map where a distance between the current altitude of the air vehicle and terrain in the map are within a second threshold. The first and second portions are updated based on a change in the current altitude of the air vehicle. In another example, a map including a projected flight path of an aircraft is displayed. Location-based information pertaining to radio frequency (RF) status between the aircraft and at least one ground radio is displayed on the map. The location-based information pertaining to RF status is updated based on a change in the current position of the air vehicle.
摘要翻译：公开了一种显示关于机动车辆的信息的方法。显示指示地图的第一部分的信息，其中航空器的当前高度与地图中的地形之间的距离在第一阈值内。显示指示地图的第二部分的信息，其中飞行器的当前高度与地图中的地形之间的距离在第二阈值内。第一和第二部分基于飞行器的当前高度的变化来更新。在另一示例中，显示包括飞行器的预计飞行路径的地图。有关飞机与至少一个地面无线电之间射频（RF）状态的位置信息显示在地图上。基于当前位置的变化来更新与RF状态有关的基于位置的信息。

7. 发明申请

WO2015031238A1 DISPLAY OF TERRAIN ALONG FLIGHT PATHS 审中-公开
标题翻译：显示飞机上的TERRAIN
公开(公告)号：WO2015031238A1
公开(公告)日：2015-03-05
申请号：PCT/US2014/052484
申请日：2014-08-25
申请人： INSITU, INC. (A SUBSIDIARY OF THE BOEING COMPANY)
发明人： HAYES, Andrew
IPC分类号： G08G5/00
CPC分类号： G05D1/0044 , B64C39/024 , B64C2201/14 , G05D1/042 , G08G5/0026 , G08G5/0069 , G08G5/0082 , G08G5/0086
摘要： Information about an air vehicle can be displayed, including a profile of terrain for a projected flight path of an aircraft. A first line at a first attitude above the profile of terrain can be displayed where the first line substantially follows the contour of the profile of terrain. A second line at a second attitude above the profile of terrain can be displayed where the second line substantially follows the contour of the profile of terrain. The display can also include an icon representing an altitude of the aircraft with respect to the profile of terrain. A third line projecting from the icon can be displayed to represent a command altitude for the projected flight path.
摘要翻译：可以显示关于飞行器的信息，包括用于飞行器的预计飞行路径的地形轮廓。可以在第一线基本上遵循地形轮廓的轮廓的情况下显示在地形轮廓之上的第一姿态的第一线。可以显示在地形轮廓之上的第二姿态的第二行，其中第二行基本上遵循地形轮廓的轮廓。显示器还可以包括表示飞机相对于地形轮廓的高度的图标。可以显示从图标突出的第三条线，以表示投影飞行路径的命令高度。

8. 发明申请

WO2011142859A1 TWO-STROKE, FUEL INJECTED INTERNAL COMBUSTION ENGINES FOR UNMANNED AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS 审中-公开
标题翻译：两用燃油喷射内燃机，用于不定型飞机及相关系统及方法
公开(公告)号：WO2011142859A1
公开(公告)日：2011-11-17
申请号：PCT/US2011/023815
申请日：2011-02-04
申请人： INSITU, INC. , FFIELD, Paul , SIMMONS, Chuck , STEBBINS, Glen
发明人： FFIELD, Paul , SIMMONS, Chuck , STEBBINS, Glen
IPC分类号： F02B25/14 , F02B25/20 , F02B33/04 , F02D41/30
CPC分类号： F02M39/00 , B64D27/08 , F02B25/14 , F02B25/20 , F02B33/04 , F02B2075/025 , F02B2075/125 , F02D35/023 , F02D41/0087 , F02D41/123 , F02D41/1439 , F02D41/1444 , F02D41/222 , F02D41/3058 , F02D2200/0404 , F02D2400/04 , F02M69/10 , Y02T10/123
摘要： Two-stroke, fuel injected internal combustion engines for unmanned aircraft and associated systems and methods are disclosed herein. Engines configured in accordance with embodiments of the disclosure can include, for example, (a) an electronic fuel injection system configured to provide a desired low fuel rate by injecting fuel every nth compression cycle rather than every cycle (so-called "skip-cycle" operation), (b) one or more pressure sensors configured to measure fluctuations in peak crankcase pressure and use such fluctuations to control fuel injection delivery, and (c) a multi-cylinder configuration having a common crankcase with a fuel injection arrangement configured to mitigate or eliminate problems with mixed redistribution.
摘要翻译：本文公开了用于无人驾驶飞行器的二冲程燃料喷射内燃机及相关系统和方法。根据本公开的实施例构造的发动机可以包括例如（a）电子燃料喷射系统，该电子燃料喷射系统被配置为通过每第n个压缩循环而不是每个周期喷射燃料来提供期望的低燃料速率（所谓的“跳过循环 “操作”），（b）一个或多个压力传感器，被配置为测量曲轴箱顶部压力的波动并使用这种波动来控制燃料喷射输送;以及（c）具有共同的曲轴箱的多气缸构造，燃料喷射装置配置成减轻或消除混合再分配的问题。

9. 发明申请

WO2009142790A1 VIBRATION ISOLATION DEVICES AND ASSOCIATED SYSTEMS AND METHODS 审中-公开
标题翻译：振动隔离装置及相关系统及方法
公开(公告)号：WO2009142790A1
公开(公告)日：2009-11-26
申请号：PCT/US2009/035320
申请日：2009-02-26
申请人： INSITU, INC. , VON FLOTOW, Andreas, H. , HORTON, Tyler, Patrick
发明人： VON FLOTOW, Andreas, H. , HORTON, Tyler, Patrick
IPC分类号： B64C1/00
CPC分类号： B64C39/024 , B64C2201/028 , B64C2201/127 , B64C2201/165
摘要： Vibration isolation devices and associated systems and methods are disclosed herein. In one embodiment, for example, an unmanned aircraft can include a fuselage having a first fuselage section and a second fuselage section adjacent to and at least approximately longitudinally aligned with the first fuselage section. The aircraft can also include at least one vibration isolation device coupling the first fuselage section to the second fuselage section. The vibration isolation device is translationally stiffer along a longitudinal axis than it is along a lateral and a vertical axis, and rotationally stiffer about a pitch and a yaw axis than it is about a roll axis.
摘要翻译：本文公开了隔振装置及相关系统和方法。在一个实施例中，例如，无人飞行器可以包括具有第一机身部分的机身和与第一机身部分相邻并且至少大致纵向对齐的第二机身部分。飞机还可以包括将第一机身部分连接到第二机身部分的至少一个隔振装置。振动隔离装置沿着纵向轴线比沿着横向轴线和垂直轴线平移地更硬，并且围绕俯仰轴线和偏转轴线旋转地比围绕辊轴线旋转更硬。

10. 发明申请

WO2015073100A1 UNMANNED VEHICLE SIMULATION 审中-公开
标题翻译：无人机模拟
公开(公告)号：WO2015073100A1
公开(公告)日：2015-05-21
申请号：PCT/US2014/053074
申请日：2014-08-28
申请人： INSITU, INC. (A SUBSIDIARY OF THE BOEING COMPANY)
发明人： HALES, Simon A. , TROWBRIDGE, Teddy T.
IPC分类号： G09B9/08 , G09B9/48
CPC分类号： G09B9/08 , G09B9/02 , G09B9/48
摘要： A method of simulating a launch of an unmanned air vehicle may include providing an interface for a user selectable launch option for a plurality of simulation modes, and responsive to a user input at the interface, simulating a launch of an unmanned air vehicle into an orbit using a predefined launch model and orbit parameters.
摘要翻译：模拟无人驾驶飞行器的发射的方法可以包括为多个模拟模式提供用于用户可选择的启动选项的接口，并且响应于界面处的用户输入，模拟将无人驾驶飞行器引入轨道使用预定义的启动模型和轨道参数。

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