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1. 发明申请

WO2006120321A2 PROCEDE D’AIDE AU DECOLLAGE D’UN AERONEF 审中-公开
标题翻译：辅助起飞方法
公开(公告)号：WO2006120321A2
公开(公告)日：2006-11-16
申请号：PCT/FR2006/001000
申请日：2006-05-04
申请人： AIRBUS FRANCE , MATHIEU, Gérard , DELAPLACE, Franck , LE TRON, Xavier
发明人： MATHIEU, Gérard , DELAPLACE, Franck , LE TRON, Xavier
IPC分类号： G05D1/08 , B64C13/16
CPC分类号： G05D1/0083 , G05D1/0661
摘要： Selon l'invention, on choisit arbitrairement une valeur de référence VRref dans la plage des vitesses de rotation possibles, on braque l'empennage horizontal réglable au moins en fonction du centrage, pour cette valeur VRref, on détermine l'écart existant entre cette valeur de référence et la valeur VC de la vitesse de l'aéronef en phase d'accélération et on agit, avant la rotation, sur les gouvernes de profondeur et/ou sur l'empennage horizontal réglable de l'aéronef (1 ) pour tenir compte dudit écart.
摘要翻译：参考值VRef可以从可能的转速的范围中任意选择，可调节水平稳定器的位置至少根据所述中心位置成角度，对于所述值VRef，所述参考值和加速飞行器速度值VC之间的偏差并且在旋转之前控制飞机的电梯和/或可调节的水平稳定器，使得考虑到所述偏差。

2. 发明申请

WO1991015827A1 PITCH GUIDANCE SYSTEM 审中-公开
标题翻译：指针系统
公开(公告)号：WO1991015827A1
公开(公告)日：1991-10-17
申请号：PCT/US1991002067
申请日：1991-03-26
申请人： SUNDSTRAND DATA CONTROL, INC.
发明人： SUNDSTRAND DATA CONTROL, INC. , GLOVER, J., Howard
IPC分类号： G06F15/50
CPC分类号： G05D1/0623 , G05D1/0661
摘要： A pitch guidance system for an aircraft utilizes inertially derived pitch information to provide the pilot with information defining the optimum pitch angle for maximum climb during a wind shear condition. The system utilizes a pitch reference modulator (22) that receives a stall warning discrete from a stall warning system to reduce the commanded pitch angle upon the occurrence of a stall warning to reduce the possibility of stalling the aircraft during degraded performance conditions such as tail winds and engine-out conditions. The system utilizes inertially derived pitch information rather than air mass derived angle of attack information to avoid transients in the angle of attack vane signal, and the commanded pitch angle is biased as a function of altitude (70) and vertical speed (58) to optimize the pitch angle for different altitudes and descent rates.
摘要翻译：用于飞行器的俯仰引导系统利用惯性导出的俯仰信息来为飞行员提供定义在风切变条件期间最大爬升的最佳俯仰角的信息。该系统使用俯仰参考调制器（22），其接收从失速警告系统离散的失速警告，以在出现失速警告时减小指令的俯仰角，以减少在退化的性能状况（例如尾风）期间使飞行器停滞的可能性和发动机的条件。该系统利用惯性导出的音调信息，而不是空气质量导出的迎角信息，以避免迎角信号的瞬变，并且指令的俯仰角作为高度（70）和垂直速度（58）的函数被偏置以优化不同高度和下降率的俯仰角。

3. 发明申请

WO2015179797A1 UNMANNED AERIAL COPTER FOR PHOTOGRAPHY AND/OR VIDEOGRAPHY 审中-公开
标题翻译：不限制的摄影和/或视频的AERIAL COPER
公开(公告)号：WO2015179797A1
公开(公告)日：2015-11-26
申请号：PCT/US2015/032240
申请日：2015-05-22
申请人： LILY ROBOTICS, INC.
发明人： BRADLOW, Henry W. , BALARESQUE, Antoine , ENGLIN, Robert N.
IPC分类号： B64C19/00 , B64C27/00 , B64C39/02 , G05D1/00
CPC分类号： G05D1/0661 , B64C19/00 , B64C27/00 , B64C27/08 , B64C39/02 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/08 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/145 , B64C2201/146 , G05D1/0022 , G05D1/0094 , G05D1/0669 , G05D1/102
摘要： Some embodiments include an unmanned aerial vehicle (UAV) copter for consumer photography or videography. The UAV copter can determine a first elevation of the UAV copter and a second elevation of an operator device. The UAV copter can adjust the first elevation by controlling thrust power of one or more propeller drivers to maintain a preset elevation difference between the first elevation and the second elevation. The UAV copter can locate a target subject relative to the UAV copter. The UAV copter can adjust at least one of the propeller drivers to point a first camera of the UAV copter at the operator device. In some embodiments, in response to detecting that the UAV copter has been thrown, the UAV copter can provide power adjustments for propeller drivers of the UAV copter to have the UAV copter reach a predetermined elevation above an operator device.
摘要翻译：一些实施例包括用于消费者摄影或摄影的无人驾驶飞行器（UAV）直升机。无人机直升机可以确定无人机直升机的第一高度和操作装置的第二高程。无人机直升机可以通过控制一个或多个螺旋桨驱动器的推力来调节第一高程，以保持第一高程和第二高程之间的预设高程差。无人机直升机可以相对于无人机直升机定位目标物体。无人机直升机可以调节至少一个螺旋桨驱动器来将无人机直升机的第一相机指向操作者设备。在一些实施例中，响应于检测到UAV直升机已被抛出，无人机直升机可以为无人机直升机的螺旋桨驱动器提供功率调节，使无人机直升机达到操作员设备上方的预定高度。

4. 发明申请

WO2006120321A3 ASSISTED TAKE-OFF METHOD FOR AIRCRAFT 审中-公开
标题翻译：辅助起飞方法
公开(公告)号：WO2006120321A3
公开(公告)日：2007-02-22
申请号：PCT/FR2006001000
申请日：2006-05-04
申请人： AIRBUS FRANCE , MATHIEU GERARD , DELAPLACE FRANCK , LE TRON XAVIER
发明人： MATHIEU GERARD , DELAPLACE FRANCK , LE TRON XAVIER
IPC分类号： G05D1/06
CPC分类号： G05D1/0083 , G05D1/0661
摘要： A reference value VRef is arbitrarily selected from the range of possible rotation speeds, the position of the trimmable horizontal stabiliser is angled at least in accordance with the centring, for said value VRef, the deviation between said reference value and the accelerating aircraft speed value VC is determined, and the elevators and/or the trimmable horizontal stabiliser of the aircraft are controlled, prior to rotation, in such a way that said deviation is taken into account.
摘要翻译：参考值VRef可以从可能的转速的范围中任意选择，可调节水平稳定器的位置至少根据所述中心位置成角度，对于所述值VRef，所述参考值和加速飞行器速度值VC之间的偏差并且在旋转之前控制飞机的电梯和/或可调节的水平稳定器，使得考虑到所述偏差。

5. 发明申请

WO2008112530A3 FLIGHT MANAGEMENT SYSTEM FOR GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE 审中-公开
标题翻译：在飞机出发期间生成可变扭矩切换的飞行管理系统
公开(公告)号：WO2008112530A3
公开(公告)日：2009-10-22
申请号：PCT/US2008056174
申请日：2008-03-07
申请人： GEN ELECTRIC , DEJONGE MICHAEL K
发明人： DEJONGE MICHAEL K
IPC分类号： G05D1/06
CPC分类号： G05D1/0661
摘要： A flight management system is provided for generating a variable thrust cutback during aircraft departure. The flight management system includes memory storing a sound exposure level limit for a navigation flight and storing expected sound exposure levels for an aircraft, and one or more inputs for receiving sensed aircraft variables including altitude and airspeed. The system also includes a processor for processing the sensed altitude and airspeed and stored sound exposure levels. The processor further computes an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels for controlling aircraft throttle during departure.
摘要翻译：提供飞行管理系统，用于在飞机起飞期间产生可变推力裁减。飞行管理系统包括存储导航飞行的声音暴露级别限制并存储飞行器的预期声音暴露水平的存储器，以及用于接收感测的飞行器变量（包括高度和空速）的一个或多个输入。该系统还包括用于处理所感测的高度和空速以及存储的声音暴露水平的处理器。处理器进一步计算出符合声音暴露水平极限的发动机推力值，其基于在起飞期间控制飞机油门的高度，空速和声音暴露水平。

6. 发明申请

WO2008100293A1 METHODS AND SYSTEMS FOR IMPLEMENTING LOCATION BASED NOISE ABATEMENT PROCEDURES 审中-公开
标题翻译：用于实施基于位置的噪声消减程序的方法和系统
公开(公告)号：WO2008100293A1
公开(公告)日：2008-08-21
申请号：PCT/US2007/022387
申请日：2007-10-19
申请人： THE BOEING COMPANY , BURNSIDE, Kevin, A.
发明人： BURNSIDE, Kevin, A.
IPC分类号： B64D31/06 , G05D1/06
CPC分类号： B64D31/06 , G05D1/0661
摘要： A method for controlling one or more of engine thrust cutback and engine thrust restoration is described which is related to aircraft environmental emissions abatement. The method comprises receiving aircraft location data from at least one navigational sensing system, comparing the aircraft location data against location data identifying an environmental emissions abatement area, and controlling at least one of thrust cutback and thrust restoration of the aircraft engines based on the comparing of aircraft location to the location of the environmental emissions abatement area.
摘要翻译：描述了一种用于控制发动机推力减少和发动机推力恢复中的一个或多个的方法，其涉及飞机环境排放减少。该方法包括从至少一个导航传感系统接收飞机位置数据，将飞行器位置数据与标识环境排放消减区域的位置数据进行比较，以及基于比较来控制飞机发动机的推力减少和推力恢复中的至少一个飞机位置到环境排放减少区域的位置。

7. 发明申请

WO2018236903A1 SYSTEMS AND METHODS FOR CHARGING UNMANNED AERIAL VEHICLES ON A MOVING PLATFORM 审中-公开
公开(公告)号：WO2018236903A1
公开(公告)日：2018-12-27
申请号：PCT/US2018/038330
申请日：2018-06-19
申请人： PLANCK AEROSYSTEMS INC.
发明人： COLLINS, Gaemus , CLAUSSE, Aubrey , TWINING, David
IPC分类号： B64C39/02
CPC分类号： G05D1/0684 , B64C39/024 , B64C2201/066 , B64C2201/141 , G05D1/0088 , G05D1/0661 , G06K9/00624 , G06K9/00637 , G06K9/3216 , G08G5/0021 , G08G5/0069 , G08G5/0073 , G08G5/025
摘要： Disclosed herein are system and method for automatically recharging a unmanned aerial vehicle (UAV) on a moving platform, comprising: a software module identifying the moving platform; a software module estimating a real-time state of the moving platform; a software module controlling automatic landing of the UAV on the moving platform based on the real-time state estimation of the moving platform and data collected from the one or more sensors; a software module controlling automatic connection of the UAV to a charging station of the moving platform with a pre-determined orientation; and a software module controlling automatic taking off of the UAV from the moving platform after charging.

8. 发明申请

WO2008112530A2 FLIGHT MANAGEMENT SYSTEM FOR GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE 审中-公开
标题翻译：在飞机出发期间生成可变扭矩切换的飞行管理系统
公开(公告)号：WO2008112530A2
公开(公告)日：2008-09-18
申请号：PCT/US2008/056174
申请日：2008-03-07
申请人： GENERAL ELECTRIC COMPANY , DEJONGE, Michael, K.
发明人： DEJONGE, Michael, K.
IPC分类号： G05D1/06
CPC分类号： G05D1/0661
摘要： A flight management system is provided for generating a variable thrust cutback during aircraft departure. The flight management system includes memory storing a sound exposure level limit for a navigation flight and storing expected sound exposure levels for an aircraft, and one or more inputs for receiving sensed aircraft variables including altitude and airspeed. The system also includes a processor for processing the sensed altitude and airspeed and stored sound exposure levels. The processor further computes an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels for controlling aircraft throttle during departure.
摘要翻译：提供飞行管理系统，用于在飞机起飞期间产生可变推力裁减。飞行管理系统包括存储导航飞行的声音暴露级别限制并存储飞行器的预期声音暴露水平的存储器，以及用于接收感测的飞行器变量（包括高度和空速）的一个或多个输入。该系统还包括用于处理所感测的高度和空速以及存储的声音暴露水平的处理器。处理器进一步计算出符合声音暴露水平极限的发动机推力值，其基于在起飞期间控制飞机油门的高度，空速和声音暴露水平。

9. 发明申请

WO0239060A2 DETECTING A LOW PERFORMANCE TAKEOFF CONDITION FOR AIRCRAFT FOR USE WITH GROUND PROXIMITY WARNING SYSTEMS 审中-公开
标题翻译：检测飞机使用地面接地警告系统的性能下降条件
公开(公告)号：WO0239060A2
公开(公告)日：2002-05-16
申请号：PCT/US0123387
申请日：2001-07-23
申请人： HONEYWELL INT INC
发明人： JOHNSON STEVEN
IPC分类号： B64D45/00 , G01C23/00 , G05D1/06 , G01C5/00
CPC分类号： G01C23/005 , G05D1/0661
摘要： The present invention includes a system, method and computer program product for reducing nuisance warnings during low performance takeoff conditions. The system includes a first component that determines aircraft current clinb rate and potential climb rate based on aircraft vertical speed data and velocity information and a second componnet that adds the determined current climb rate and potential climb rate. The system also includes a third component that disables alerts, if the sum of the current climb rate and potential climb rate differ from a predetermined climb rate by a threshold amount and if the aircraft is supposed to be in a maximum thrust condition (e.g. takeoff, missed approach).
摘要翻译：本发明包括一种用于在低性能起飞条件下减少有害警告的系统，方法和计算机程序产品。该系统包括基于飞机垂直速度数据和速度信息确定飞机当前临时速率和潜在爬升速率的第一部件，以及添加确定的当前爬升速率和潜在爬升速率的第二组件。如果当前爬升率和潜在爬升速率的总和与预定的爬升速率相差阈值量，并且如果飞行器应该处于最大推力条件（例如起飞），则该系统还包括禁用警报的第三组件，错过的方法）。

10. 发明申请

WO2008112527A3 METHOD OF GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE 审中-公开
标题翻译：在飞机出发时产生可变扭矩的方法
公开(公告)号：WO2008112527A3
公开(公告)日：2009-10-22
申请号：PCT/US2008056170
申请日：2008-03-07
申请人： GEN ELECTRIC , DEJONGE MICHAEL K
发明人： DEJONGE MICHAEL K
IPC分类号： G05D1/06
CPC分类号： G05D1/0661
摘要： A method of producing a variable thrust cutback of an aircraft during aircraft departure is provided. The method includes the steps of storing expected sound exposure levels for an aircraft in memory, and storing a sound exposure level limit for a navigation flight in memory. The method also includes the steps of determining aircraft altitude and determining aircraft airspeed. The method further includes the steps of computing an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels, and outputting the computed engine thrust value for use in controlling the aircraft during departure.
摘要翻译：提供了一种在飞机起飞期间生产飞机可变推力裁减的方法。该方法包括以下步骤：将存储器中的飞行器的预期声音曝光水平存储在存储器中，并将导航飞行的声音曝光水平限制存储在存储器中。该方法还包括确定飞机高度并确定飞机空速的步骤。该方法还包括以下步骤：基于高度，空速和声音暴露水平计算符合声音暴露水平极限的发动机推力值，并输出计算出的发动机推力值以用于在起飞期间控制飞行器。

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