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81. 发明申请

US20140025238A1 System and Method for Multiple Aircraft Lifting a Common Payload 有权
标题翻译：多台飞机提升公共有效载荷的系统和方法
公开(公告)号：US20140025238A1
公开(公告)日：2014-01-23
申请号：US13750384
申请日：2013-01-25
申请人： Wilfred SO , Justin Eichel , Linda Vu , Peter Szabo
发明人： Wilfred SO , Justin Eichel , Linda Vu , Peter Szabo
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , B64C39/024 , B64C2201/128 , B64C2201/146 , B64D1/22 , G05D1/104
摘要： A system and method are provided for controlling a plurality of aircraft to lift a common payload. The system comprises of multiple aircraft tethered to a common payload, where the group of aircraft form a swarm that is controlled by a pilot station. Each aircraft is autonomously stabilized and guided through a swarm avionics unit, which further includes sensor, communication, and processing hardware. At the pilot station, a pilot remotely enters payload destinations, which is processed and communicated to each aircraft. The method for controlling a multi-aircraft lifting system includes of inputting the desired location of the payload, and determining a series of intermediary payload waypoints. Next, these payload waypoints are used by the swarm waypoint controller to generate individual waypoints for each aircraft. A flight controller for each aircraft moves the aircraft to these individual waypoints.
摘要翻译：提供了一种用于控制多个飞机以提升公共有效载荷的系统和方法。系统包括连接到公共有效载荷的多个飞机，其中飞机组形成由飞行员站控制的群。每架飞机自主稳定，并通过一个群组航空电子设备进行引导，该单元还包括传感器，通讯和处理硬件。在试点站，飞行员远程进入有效载荷目的地，并对每个飞机进行处理和传送。用于控制多机提升系统的方法包括输入有效载荷的期望位置，以及确定一系列中间有效载荷航路点。接下来，这些有效载荷航路点由群组航点控制器用于为每个飞机生成单独的航路点。每架飞机的飞行控制器将飞机移动到这些单独的航路点。

82. 发明授权

US08600602B1 Flight technical control management for an unmanned aerial vehicle 失效
公开(公告)号：US08600602B1
公开(公告)日：2013-12-03
申请号：US13932623
申请日：2013-07-01
申请人： Honeywell International Inc.
发明人： Katherine McAndrew , Linda J. Watson , Jon Feist , A. Christopher Moorman
IPC分类号： G01C22/00 , B64C13/16 , G09B9/08
CPC分类号： B64C19/00 , G05D1/0038 , G05D1/0077 , G05D1/0088
摘要： Two architectures for unmanned aerial vehicles (UAVs) and a method for executing a mission plan are provided. One architecture for a UAV includes a flight command and mission execution (FCME) component making strategic decisions, a flight technical control manager (FTCM) making tactical decisions and a vehicle management system (VMS) providing navigational support. The FCME and FTCM execute on one processor and the VMS executes on a separate processor. The second architecture includes redundant processors for executing the FCME and FTCM as well as redundant processors for executing the VMS. The UAV executes a mission plan, which may include flight plan(s), communication plan(s), weapons plan(s), sensor plan(s), and/or contingent flight plan(s). The UAV may control various optical sensors, training sensors, and lights as well.

83. 发明申请

US20130317667A1 AUTOMATIC FLIGHT CONTROL FOR UAV BASED SOLID MODELING 有权
公开(公告)号：US20130317667A1
公开(公告)日：2013-11-28
申请号：US13054882
申请日：2010-09-30
申请人： Ezekiel Kruglick
发明人： Ezekiel Kruglick
IPC分类号： B64C19/00
CPC分类号： B64C39/024 , B64C19/00 , B64C2201/127 , B64C2201/141 , B64C2201/146 , G05D1/0088 , G05D1/0094 , G05D1/101 , G06T17/05 , G06T17/10 , G06T2210/21 , G06T2210/61
摘要： Technologies are generally described for controlling a flight path of a UAV based image capture system for solid modeling. Upon determining an initial movement path based on an estimate of a structure to be modeled, images of the structure to be modeled may be captured and surface hypotheses formed for unobserved surfaces based on the captured images. A normal vector and a viewing cone may be computed for each hypothesized surface. A set of desired locations may be determined based on the viewing cones for the entire structure to be modeled and a least impact path for the UAV determined based on the desired locations and desired flight parameters.

84. 发明申请

US20130274965A1 AUTOMATED TAKE OFF CONTROL SYSTEM AND METHOD 审中-公开
标题翻译：自动关闭控制系统和方法
公开(公告)号：US20130274965A1
公开(公告)日：2013-10-17
申请号：US13846532
申请日：2013-03-18
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Scot Griffith , Kent Stange
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , G05D1/0661
摘要： Methods and systems for operating an avionics system on-board an aircraft are provided. In one embodiment, data associated with a take off roll is received, one or more v-speeds of the aircraft associated with the take off roll are calculated, and during the take off roll, the aircraft is controlled based on the one or more calculated v-speeds.
摘要翻译：提供了在飞机上运行航空电子系统的方法和系统。在一个实施例中，接收与取出辊相关联的数据，计算与取出辊相关联的飞行器的一个或多个v速度，并且在起飞辊期间，飞行器基于一个或多个计算的 v速度。

85. 发明申请

US20130268146A1 METHOD AND A DEVICE FOR ADAPTING THE MAN-MACHINE INTERFACE OF AN AIRCRAFT DEPENDING ON THE LEVEL OF THE PILOT'S FUNCTIONAL STATE 有权
标题翻译：方法和装置，用于根据飞行员功能状态的水平来适应飞机的机器接口
公开(公告)号：US20130268146A1
公开(公告)日：2013-10-10
申请号：US13803270
申请日：2013-03-14
申请人： EUROCOPTER
发明人： Jean-Pierre Baudry
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , A61B5/18 , B64D45/00 , G01C23/00 , G06F3/011
摘要： A method of adapting a man-machine interface (20) of an aircraft (50) depending on the functional level of a pilot, the method comprising a plurality of successive steps. Firstly, before starting a mission, the characteristics of said mission and the characteristics and the physiological state of said pilot are determined. Thereafter, during said mission, the state of the mission and the current state of said aircraft together with a current behavior of said pilot are determined and a current functional level of said pilot is estimated. Thereafter, said current functional level of said pilot is compared with reference functional levels, and said man-machine interface (20) is then adapted in order to assist said pilot automatically and in optimum manner in making the pilot aware of the situation, in the pilot's decision-making, or in the actions taken by the pilot depending on the pilot's stress state or work load state.
摘要翻译：一种根据飞行员的功能水平来适应飞行器（50）的人机界面（20）的方法，该方法包括多个连续的步骤。首先，在开始任务之前，确定所述任务的特征以及所述飞行员的特征和生理状态。此后，在所述任务期间，确定所述飞行器的任务状态和当前状态以及所述导频的当前行为，并且估计所述导频的当前功能级别。此后，将所述导频的所述当前功能电平与参考功能电平进行比较，然后适配所述人机界面（20），以便在所述飞行员自动地和以最佳方式使驾驶员了解该情况时，在飞行员的决策或飞行员根据飞行员的压力状态或工作负载状态采取的行动。

86. 发明申请

US20130253733A1 COMPUTING DEVICE AND METHOD FOR CONTROLLING UNMANNED AERIAL VEHICLE IN FLIGHT SPACE 有权
标题翻译：用于在空中空间中控制不必要的空中航空器的计算装置和方法
公开(公告)号：US20130253733A1
公开(公告)日：2013-09-26
申请号：US13674959
申请日：2012-11-13
申请人： HON HAI PRECISION INDUSTRY CO., LTD.
发明人： HOU-HSIEN LEE , CHANG-JUNG LEE , CHIH-PING LO
IPC分类号： B64C19/00
CPC分类号： G07C5/008 , B64C19/00 , B64C39/024 , B64C2201/146 , G05D1/0016 , G05D1/0202 , G06F3/017 , G06T2207/10016
摘要： In a method for controlling an unmanned aerial vehicle (UAV) in a flight space using a computing device, a 3D sample database is created and store in a storage device of the computing device. The computing device includes a depth-sensing camera that captures a 3D scene image of a scene in front of a user, and senses a depth distance between the user and the depth-sensing camera. A 3D person image of the user is detected from the 3D scene image, and gesture information of the user is obtained by comparing the 3D person image with human gesture data stored in the 3D sample database. The method converts the gesture information of the user into one or more flight control commands, and drives a driver of the UAV to control the UAV to fly in a flight space according to the flight control commands
摘要翻译：在使用计算设备控制飞行空间中的无人机（UAV）的方法中，创建3D样本数据库并存储在计算设备的存储设备中。计算装置包括深度感测相机，其捕获用户前面的场景的3D场景图像，并感测用户和深度感测相机之间的深度距离。从3D场景图像检测用户的3D人物图像，并且通过将3D人物图像与存储在3D样本数据库中的人类手势数据进行比较来获得用户的手势信息。该方法将用户的手势信息转换成一个或多个飞行控制命令，并且驱动无人机的驾驶员以根据飞行控制命令控制无人机飞行在飞行空间中

87. 发明申请

US20130248656A1 INTEGRATED WAFER SCALE, HIGH DATA RATE, WIRELESS REPEATER PLACED ON FIXED OR MOBILE ELEVATED PLATFORMS 审中-公开
标题翻译：集成式WAFER SCALE，高数据速率，无缝重新安装在固定或移动平台上
公开(公告)号：US20130248656A1
公开(公告)日：2013-09-26
申请号：US13722868
申请日：2012-12-20
申请人： Farrokh Mohamadi
发明人： Farrokh Mohamadi
IPC分类号： H04W16/00 , B64C19/00
CPC分类号： H04B7/1555 , B64C19/00 , B64C39/024 , B64C2201/122 , B64C2201/141 , B64C2201/146 , H04B7/18504 , H04B7/2606 , H04W16/00 , H04W16/26 , H04W16/28 , H04W72/046
摘要： Methods and systems are provided for relocatable repeaters for wireless communication links to locations that may present accessibility problems using, for example, small unmanned aerial systems (sUAS). An sUAS implemented as an easy-to-operate, small vertical take-off and landing (VTOL) aircraft with hovering capability for holding station position may provide an extended range, highly secure, high data rate, repeater system for extending the range of point-to-point wireless communication links (also referred to as “crosslinks”) in which repeater locations are easily relocatable with very fast set-up and relocating times. A repeater system using beam forming and power combining techniques enables a very high gain antenna array with very narrow beam width and superb pointing accuracy. The aircraft includes a control system enabling three-dimensional pointing and sustaining directivity of the beam independently of flight path of the aircraft.
摘要翻译：为可重定位中继器提供方法和系统，用于到可能使用例如小型无人空中系统（sUAS）呈现可及性问题的位置的无线通信链路。作为一种易于操作的小型垂直起降飞机（VTOL）飞机实现的sUAS可以提供扩展范围，高度安全，高数据速率的中继器系统，用于扩展点的范围点对点无线通信链路（也称为“交叉”），其中中继器位置可以以非常快的建立和重定位时间容易地重新定位。使用波束形成和功率组合技术的中继器系统能够实现非常高的增益天线阵列，其具有非常窄的波束宽度和极好的指向精度。该飞机包括一个控制系统，能够独立于飞行器飞行路径的三维指向和维持梁的方向性。

88. 发明申请

US20130197727A1 METHOD AND DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING A LANDING PHASE 有权
标题翻译：用于在陆地阶段中为飞机提供辅助的方法和装置
公开(公告)号：US20130197727A1
公开(公告)日：2013-08-01
申请号：US13748252
申请日：2013-01-23
申请人： AIRBUS OPERATIONS (S.A.S.)
发明人： Jean MULLER , Malika ESSADOUNI
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , B64C25/426 , G05D1/0083
摘要： Method and device for aiding the piloting of an airplane during a landing phase for ensuring, during rollout on a landing runway, that in the nominal case the airplane will stop level with a selected exit, while guaranteeing that in the case of a fault the airplane will stop before the end of the runway.
摘要翻译：在着陆阶段帮助驾驶飞机的方法和装置，以确保在着陆跑道上推出时，在标称情况下，飞机将以选定的出口停止水平，同时保证飞机在发生故障的情况下将在跑道结束之前停止。

89. 发明申请

US20130144518A1 Method, Device and System for Guaranteeing a Temporal Spacing Between an Aircraft and At Least One Reference Moving Object 有权
标题翻译：用于确保飞机与至少一个参考移动物体之间的时间间隔的方法，装置和系统
公开(公告)号：US20130144518A1
公开(公告)日：2013-06-06
申请号：US13705621
申请日：2012-12-05
申请人： THALES
发明人： Benoit DACRE-WRIGHT , Guy DEKER
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , G08G5/0021 , G08G5/0039 , G08G5/0043 , G08G5/0078
摘要： A method is provided for guaranteeing a temporal spacing between an aircraft and at least one reference moving object, said spacing needing to be guaranteed no later than at a point in the flight plan called the point of interception, with the aircraft following a current flight plan. The feasibility of guaranteeing the spacing at a date Tcour by regulating the speed of the aircraft while maintaining the current flight plan is verified in a first step. In a second step it is verified whether the date Tcour is contained within a feasibility range. In a third step the current flight plan is modified when the feasibility is not verified, a lateral trajectory between the current position Xcour of the aircraft and the point of interception being implemented in this case such that the spacing can be attained by regulating the speed.
摘要翻译：提供了一种用于保证飞行器与至少一个参考移动物体之间的时间间隔的方法，所述间距需要不迟于在称为拦截点的飞行计划中的一点保证，飞机遵循当前飞行计划。在第一步中验证了通过在保持当前飞行计划的同时调节飞机的速度来保证时间间隔的可行性。在第二步中，验证日期Tcour是否包含在可行范围内。在第三步中，当可行性未得到验证时，当前飞行计划被修改，在这种情况下在飞行器的当前位置Xcour和截取点之间的横向轨迹可以通过调节速度来实现。

90. 发明申请

US20130054055A1 METHOD AND SYSTEM FOR INTEGRATING ENGINE CONTROL AND FLIGHT CONTROL SYSTEM 有权
标题翻译：集成发动机控制和飞行控制系统的方法和系统
公开(公告)号：US20130054055A1
公开(公告)日：2013-02-28
申请号：US13221102
申请日：2011-08-30
申请人： Harry Kirk Mathews, JR. , Sridhar Adibhatla , Jeffrey Russell Bult
发明人： Harry Kirk Mathews, JR. , Sridhar Adibhatla , Jeffrey Russell Bult
IPC分类号： G05D1/00 , G06F19/00
CPC分类号： B64C19/00 , B64D31/06 , F05D2260/80 , H04B7/18506
摘要： A method and system of operating an aircraft system are provided. The aircraft system includes an integrated aircraft flight control system that includes an engine control system configured to generate engine performance and health information. The integrated aircraft flight control system also includes a flight control system configured to generate flight information and trajectory intent information. The integrated aircraft flight control system further includes a communications channel communicatively coupled between the engine control system and the flight control system, where the engine control system is configured to transmit the generated engine performance and health information to the flight control system using the communications channel and the flight control system is configured to transmit the generated flight information and trajectory intent information to the engine control system using the communications channel.
摘要翻译：提供了一种操作飞行器系统的方法和系统。该飞行器系统包括集成的飞行器飞行控制系统，其包括被配置为产生发动机性能和健康信息的发动机控制系统。综合飞行器飞行控制系统还包括配置成产生飞行信息和轨迹意图信息的飞行控制系统。集成飞行器飞行控制系统还包括通信地耦合在发动机控制系统和飞行控制系统之间的通信通道，其中发动机控制系统被配置为使用通信通道向飞行控制系统发送生成的发动机性能和健康信息，以及飞行控制系统被配置为使用通信信道将所生成的飞行信息和轨迹意图信息发送到引擎控制系统。

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