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51. 发明申请

US20160139603A1 AUTOMATIC TAKE-OFF AND LANDING CONTROL DEVICE 有权
标题翻译：自动起飞和着陆控制装置
公开(公告)号：US20160139603A1
公开(公告)日：2016-05-19
申请号：US14940353
申请日：2015-11-13
申请人： Airbus Defence and Space GmbH
发明人： Christiano BIANCHI , Winfried LOHMILLER
IPC分类号： G05D1/10 , G08G5/02 , G08G5/00 , B64C39/02 , B64D47/08
CPC分类号： G05D1/101 , B64C39/024 , B64D47/08 , G01S19/48 , G05D1/0653 , G08G5/0021 , G08G5/0065 , G08G5/0069 , G08G5/025
摘要： An automatic take-off and landing control device for an aircraft is provided. The control device comprises at least two of at least one local tracking device adapted for receiving at least one local signal from at least one local ground station and for determining a position of the aircraft based on the local signals, at least one GNSS tracking device adapted for receiving a GNSS signal and for determining a position of the aircraft based on the GNSS signal; and at least one camera device adapted for observing an environment of the aircraft and for determining a position of the aircraft based on the camera signal.
摘要翻译：提供了一种用于飞机的自动起飞和着陆控制装置。所述控制装置包括至少一个本地跟踪装置中的至少两个，其适于从至少一个本地地面站接收至少一个本地信号，并且用于基于所述本地信号确定所述飞行器的位置，所述至少一个GNSS跟踪装置适于用于接收GNSS信号并根据GNSS信号确定飞行器的位置; 以及至少一个相机装置，适于观察飞行器的环境并且用于基于相机信号确定飞行器的位置。

52. 发明授权

US08849481B1 GPS carrier-phase based relative navigation 有权
标题翻译： GPS载波相位相对导航
公开(公告)号：US08849481B1
公开(公告)日：2014-09-30
申请号：US13835847
申请日：2013-03-15
申请人： Vladislav Gavrilets , Patrick Hwang , Gary McGraw
发明人： Vladislav Gavrilets , Patrick Hwang , Gary McGraw
IPC分类号： G01S19/43 , G05D1/02
CPC分类号： G01C21/20 , G01S19/01 , G01S19/43 , G01S19/50 , G05D1/042 , G05D1/0653 , G05D1/0808
摘要： Systems and methods for navigation of a vehicle may carry out one or more operations including, but not limited to: obtaining coordinates of a vector connecting two points in space using carrier phase measurements from global navigation system satellites (GNSS); setting the vector as an intended path of a vehicle; storing carrier phase signals from a GNSS receiver received at a first position of the vehicle; receiving carrier phase signals from a GNSS receiver at a second position of the vehicle; and determining a position of the vehicle relative to the intended path from one or more carrier phase signals received at the second position and one or more stored carrier phase signals received at the first position.
摘要翻译：用于车辆导航的系统和方法可以执行一个或多个操作，包括但不限于：使用来自全球导航系统卫星（GNSS）的载波相位测量获得连接空间中的两个点的向量的坐标; 将矢量设置为车辆的预期路径; 存储来自在所述车辆的第一位置处接收的GNSS接收器的载波相位信号; 在车辆的第二位置处接收来自GNSS接收器的载波相位信号; 以及从在所述第二位置处接收的一个或多个载波相位信号和在所述第一位置处接收到的一个或多个存储的载波相位信号确定所述车辆相对于所述预期路径的位置。

53. 发明申请

US20030107499A1 Visual display of ground collision avoidance devices for aircraft 审中-公开
标题翻译：可视显示飞机的地面碰撞避免装置
公开(公告)号：US20030107499A1
公开(公告)日：2003-06-12
申请号：US10129089
申请日：2002-09-30
发明人： Gerard Lepere , Hugues Meunier
IPC分类号： G08B021/00
CPC分类号： G01C5/005 , G05D1/0653
摘要： The invention concerns a device designed to be installed on board an aircraft to provide eventual warning data corresponding to a risk of collision between the aircraft and the landform. The device comprises an assist-module (4) designed to use static and dynamic parameters of the aircraft with a database of the relief of the terrain flown over (3), and a visual display module (5) for displaying (55) a representation of the relief over a displayed domain, and inserting therein a particular signalling of possible warnings in particular based on a detected landing/take-off phase state.
摘要翻译：本发明涉及一种被设计为安装在飞机上的装置，以提供对应于飞机与地形之间的碰撞风险的最终警告数据。该设备包括辅助模块（4），其被设计成使用飞行器的静态和动态参数与数据库（3）的地形的浮雕数据库，以及可视显示模块（5），用于显示（55）在所显示的域中的缓解，并且特别地基于检测到的着陆/起飞阶段状态在其中插入可能的警告的特定信号。

54. 发明授权

US4488235A Speed control system for aircraft 失效
标题翻译：飞机速度控制系统
公开(公告)号：US4488235A
公开(公告)日：1984-12-11
申请号：US317823
申请日：1981-11-03
申请人： Harry Miller
发明人： Harry Miller
IPC分类号： G05D13/62 , B64C13/18 , G05D1/06 , G05D13/00 , G05D1/08 , G06G7/66
CPC分类号： G05D1/0638 , G05D1/0653
摘要： Speed control apparatus for use in an aircraft performance management system of the type wherein a target Mach number command is supplied to the aircraft pitch controls to attain the target Mach and is simultaneously supplied to the aircraft throttles to capture a computed engine pressure ratio (EPR) or fan speed (N.sub.1), said apparatus being operative during maximum thrust climbs and minimum thrust descents upon an abrupt step function target Mach number command wherein said step function command is converted to a ramp command, the slope of which is directly proportional to the existing thrust-minus-drag conditions of the aircraft and inversely proportional to its existing weight, thus ensuring a proper division between aircraft acceleration and rate of climb or aircraft deceleration and rate of descent.
摘要翻译：用于飞机性能管理系统的速度控制装置，其中向飞行器俯仰控制提供目标马赫数指令以实现目标马赫，同时提供给飞行器节流阀以捕获计算的发动机压力比（EPR）或风扇速度（N1），所述装置在突然步骤功能目标马赫数指令的最大推力爬升和最小推力下降期间操作，其中所述步进功能命令被转换成斜坡命令，其斜率与现有的飞机的推力 - 负阻力条件与其现有重量成反比，从而确保飞机加速度与爬升速度或飞机减速度和下降速率之间的适当分配。

55. 发明授权

US4042197A Automatic controls for airplane take-off and landing modes 失效
标题翻译：飞机起飞和着陆模式的自动控制
公开(公告)号：US4042197A
公开(公告)日：1977-08-16
申请号：US617621
申请日：1975-09-29
申请人： James Alfred Boyle , Peteris Adams Galins , Mark Charles Gregoire , Peter L. M. O'Toole
发明人： James Alfred Boyle , Peteris Adams Galins , Mark Charles Gregoire , Peter L. M. O'Toole
IPC分类号： G05D1/06 , G05D1/12
CPC分类号： G05D1/0653
摘要： A take-off and landing control device for automatic retraction of flaps upon stowing landing gear and upon attaining a predetermined airspeed and of indicating distance from brake release during take-off, and for an automatic decelerating approach with flaps extending as a function of distance from touchdown with automatic throttle cutback and automatic stabilizer trim in response to flap location maintaining an essentially constant angle of attack.
摘要翻译：一种起降落地控制装置，用于在起落架上自动缩回襟翼，并且在获得预定空速并且在起飞期间指示与制动器释放之间的距离以及用于作为距离的距离延伸的襟翼的自动减速方法触控屏幕具有自动节气门裁切功能，并且响应于挡板位置的自动稳定器装饰，保持基本上恒定的迎角。

56. 发明授权

US2322225A Aircraft automatic take-off, flight, and landing 失效
标题翻译：飞机自动起飞，飞行和着陆
公开(公告)号：US2322225A
公开(公告)日：1943-06-22
申请号：US28731039
申请日：1939-07-29
申请人： CRANE CARL J , HOLLOMAN GEORGE V , STOUT RAYMOND K , BARBULESCO CONSTANTIN D
发明人： CRANE CARL J , HOLLOMAN GEORGE V , STOUT RAYMOND K , BARBULESCO CONSTANTIN D
IPC分类号： G05D1/06
CPC分类号： G05D1/0653

57. 发明专利

JP2013086795A Method for noise abatement procedure for an aircraft 有权
标题翻译：航空器噪声消除程序的方法
公开(公告)号：JP2013086795A
公开(公告)日：2013-05-13
申请号：JP2012227562
申请日：2012-10-15
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： BAKKER MICHAEL JOHN , HOCHWARTH JOACHIM KARL ULF , FLANARY SEAN EDWARD
IPC分类号： B64C13/18 , G08G5/00
CPC分类号： G05D1/0653 , G08G5/006
摘要： PROBLEM TO BE SOLVED: To provide a method of reducing noise from an aircraft in a noise abatement zone during flight of the aircraft.SOLUTION: The method includes determining where the flight path of the aircraft will intersect the noise abatement zone 34 and then operating the aircraft in a quieter manner when the aircraft is within the noise abatement zone 34.
摘要翻译：要解决的问题：提供一种在飞行器飞行期间减少噪声消除区域中的飞机噪声的方法。解决方案：该方法包括确定飞行器的飞行路径在噪声消除区域34的何处与航空器处于噪声消除区域34内的情况下以更安静的方式操作飞行器的位置。版权所有（C））2013，JPO＆INPIT

58. 发明专利

JP2008290704A Method for vertical takeoff from and landing on inclined surfaces 审中-公开
标题翻译：在垂直表面上垂直剥离和着陆的方法
公开(公告)号：JP2008290704A
公开(公告)日：2008-12-04
申请号：JP2008042051
申请日：2008-02-22
申请人： Honeywell Internatl Inc , ハネウェル・インターナショナル・インコーポレーテッド
发明人： HURSIG DAVID C , MARTINEZ STEVEN D
IPC分类号： B64C25/32 , B64C29/00
CPC分类号： B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/088 , B64C2201/108 , B64C2201/162 , B64D45/04 , G05D1/0653 , G05D1/0858
摘要： PROBLEM TO BE SOLVED: To provide an unmanned air vehicle capable of performing vertical takeoff from and landing on inclined surfaces.
SOLUTION: Takeoff and landing modes are added to a flight control system of a Vertical Take-Off and Landing (VTOL) Unmanned Air Vehicle (UAV). The takeoff and landing modes use data available to the flight control system and the VTOL UAV's existing control surfaces and throttle control. As a result, the VTOL UAV can takeoff from and land on inclined surfaces without the use of landing gear mechanisms designed to level the UAV on the inclined surfaces.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供能够在倾斜表面上执行垂直起飞和着陆的无人驾驶飞行器。
解决方案：起飞和着陆模式被添加到垂直起飞和着陆（VTOL）无人机（UAV）的飞行控制系统。起飞和着陆模式使用可用于飞行控制系统和VTOL无人机现有控制面和节气门控制的数据。因此，VTOL无人机可以在倾斜的表面上起飞和着陆，而不需要使用设计成在倾斜表面上对无人机进行平坦化的起落架机构。版权所有（C）2009，JPO＆INPIT

59. 发明专利

JP2005297922A Automatic takeoff device of airplane, automatic landing device, automatic takeoff/landing device, and automatic takeoff method of airplane, automatic landing method, and automatic takeoff/landing method 有权
标题翻译：机动自动起落装置，自动起落装置，自动起落架装置，自动起落方式，自动起落方式，自动起落方式
公开(公告)号：JP2005297922A
公开(公告)日：2005-10-27
申请号：JP2004120814
申请日：2004-04-15
申请人： Fuji Heavy Ind Ltd , 富士重工業株式会社
发明人： YAMANE AKIHIRO
IPC分类号： B64C13/18 , B64D45/04 , G05D1/06 , G08G5/02
CPC分类号： G05D1/0653 , B64C13/18
摘要： PROBLEM TO BE SOLVED: To accomplish full-automatic takeoff and/or full-automatic landing of an airplane without using any complicated on-board apparatus or control logic.
SOLUTION: The automatic takeoff and landing devices of an airplane are equipped with sensors 2-6 to sense the terrain clearance of the airplane, air speed, attitude angle, flying azimuth, and the position, a means to enter a takeoff/landing command, and a control device 12 to control a propulsive device and/or maneuvering device 8-10 of the airplane 1 on the basis of the information concerning the airplane 1 and the takeoff/landing command. The control device 12 makes a transfer from the takeoff run control to the nose-up control when the air speed of the airplane 1 has exceeded the specified takeoff judging speed, and transfers from the nose-up control to the crime control when the terrain clearance of the airplane 1 has exceeded the specified takeoff judging altitude. Also the control device 12 makes a transfer from the approach control to the pull-out control when the terrain clearance of the airplane 1 has become below the specified landing judging altitude and transfers from the pull-out control to the landing roll control when the air speed of the airplane 1 has become below the specified landing judging speed.
COPYRIGHT: (C)2006,JPO&NCIPI
摘要翻译：要解决的问题：实现飞机的全自动起飞和/或全自动着陆，而不使用任何复杂的车载设备或控制逻辑。
解决方案：飞机的自动起飞和着陆装置配备有传感器2-6以感测飞机的地形间隙，空气速度，姿态角，飞行方位角和位置，进入起飞/ 基于有关飞机1的信息和起飞/着陆命令来控制飞机1的推进装置和/或机动装置8-10的控制装置12。当飞机1的空气速度超过规定的起飞判断速度时，控制装置12进行从起飞行驶控制向起飞控制的转移，并且当地形间隙的飞机1已经超过了指定的起飞判定高度。此外，当飞机1的地形间隙已经变得低于指定的着陆判定高度时，控制装置12进行从进近控制到拉出控制的转移，并且当空气流动时，从拉出控制转移到降落辊控制飞机1的速度已经低于指定的着陆判断速度。版权所有（C）2006，JPO＆NCIPI

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