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    Aircraft precision approach and shipboard landing control system and method
    2.
    发明授权
    Aircraft precision approach and shipboard landing control system and method 有权
    飞机精密方法和船上着陆控制系统及方法

    公开(公告)号：US09547991B2

    公开(公告)日：2017-01-17

    申请号：US13901089

    申请日：2013-05-23

    申请人： HONEYWELL INTERNATIONAL INC.

    发明人： Michael Ray Elgersma ,  Xiaohong Linda Li

    IPC分类号： G06F19/00 ,  G06G7/70 ,  G08G5/02 ,  G05D1/06 ,  G05D1/12 ,  B64F1/00 ,  G05D1/00 ,  B64C13/16

    CPC分类号： G08G5/025 ,  B64C13/16 ,  B64F1/00 ,  G05D1/00 ,  G05D1/0684 ,  G06F19/00 ,  G06G7/70 ,  G08G5/02

    摘要： A system and method of generating a landing trajectory for use in landing an aircraft onto a deck of a waterborne ship includes sensing motion of the ship, and sensing wind speed and wind direction. The sensed motion of the ship is processed to generate estimates of ship attitude and vertical speed, and the sensed wind speed and wind direction are processed to generate estimates of air-wake disturbances ahead of the aircraft. The landing trajectory is generated based on the estimates of ship attitude and vertical speed and the estimates of air-wake disturbances. The system and method implement model predictive control to calculate the control maneuvers multiple steps ahead, which provides the capability to smoothly control the timing of the aircraft touchdown phase.

    摘要翻译： 一种生成用于将飞机着陆在水上船的甲板上的着陆轨迹的系统和方法包括感测船舶的运动，以及感测风速和风向。 对船舶的感测运动进行处理以产生船舶姿态和垂直速度的估计，并且处理感测到的风速和风向以产生飞机之前的空气 - 苏醒干扰的估计。 基于船舶姿态和垂直速度的估计以及空气 - 尾流扰动的估计值来生成着陆轨迹。 该系统和方法实现模型预测控制，以计算控制操纵前进多个步骤，提供平滑控制飞机着陆阶段时间的能力。

    Determining a Profile for an Aircraft Prior to Flight Using a Fuel Vector and Uncertainty Bands
    3.
    发明申请
    Determining a Profile for an Aircraft Prior to Flight Using a Fuel Vector and Uncertainty Bands 有权
    使用燃料矢量和不确定性带确定飞行前的飞机的轮廓

    公开(公告)号：US20150148992A1

    公开(公告)日：2015-05-28

    申请号：US14088682

    申请日：2013-11-25

    申请人： AeroData, Inc.

    发明人： Terry L. McDonough ,  Magnus Kernast ,  Carlos E. Padilla ,  Shane C. Tillotson

    IPC分类号： G08G5/00 ,  G06G7/70

    CPC分类号： G06G7/70 ,  B64F5/00 ,  G01M1/122 ,  G01M1/125 ,  G01M1/127

    摘要： A weight and center-of-gravity profile for an aircraft is determined prior to flight. An uncertainty band is determined for each of a plurality of points along a fuel vector for the planned flight. Each of the points along the fuel vector is compared to a predetermined flight limit (e.g., an FAA certified envelope). This comparison is used to decide whether the profile is suitable for flight of the aircraft. If so, an indication is provided to a user (e.g., on a display or by a text message) that the profile is suitable and the aircraft is ready for flight.

    摘要翻译： 在飞行前确定飞机的重量和重心剖面。 沿着用于计划飞行的燃料矢量的多个点中的每个点确定不确定性带。 将沿着燃料矢量的每个点与预定的飞行限制（例如，FAA认证的信封）进行比较。 该比较用于确定轮廓是否适合飞行器的飞行。 如果是这样，则向用户（例如，在显示器上或通过文本消息）提供该配置文件是合适的并且飞机准备好飞行的指示。

    Determination of non-uniformities of loaded wheels by load simulation
    4.
    发明授权
    Determination of non-uniformities of loaded wheels by load simulation 有权
    通过负载模拟确定负载车轮的非均匀性

    公开(公告)号：US08793109B2

    公开(公告)日：2014-07-29

    申请号：US13280834

    申请日：2011-10-25

    申请人： Paolo Sotgiu ,  Francesco Braghiroli ,  Marco Tralli

    发明人： Paolo Sotgiu ,  Francesco Braghiroli ,  Marco Tralli

    IPC分类号： G06G7/48

    CPC分类号： G01M17/027 ,  G06F17/5009 ,  G06F17/5095 ,  G06F2217/16 ,  G06G7/70

    摘要： The invention relates to a method for contactless determining non-uniformities of a loaded wheel, comprising the steps of determining outer contour of at least a portion of the unloaded wheel; simulating loading of the wheel with a virtual loading element bearing against the tire tread for a plurality of rotary positions of the wheel on the basis of the determined outer contour, a displacement of the determined outer contour caused by the virtual loading element and a predetermined spring rate associated to the tire tread; and determining non-uniformities of the loaded wheel using the simulation results.

    摘要翻译： 本发明涉及一种用于非接触式确定装载轮的非均匀性的方法，包括以下步骤：确定所述无载轮的至少一部分的外轮廓; 基于所确定的外轮廓，模拟车轮的负载，其中虚拟加载元件基于所确定的外轮廓而承载抵靠轮胎胎面的多个旋转位置，由虚拟加载元件引起的所确定的外轮廓的位移和预定弹簧 与轮胎胎面相关的速率; 并使用模拟结果确定装载的车轮的不均匀性。

    Apparatus for determining the phase difference between the rolling oscillation of a ship and a liquid contained in a stabilizing tank
    7.
    发明授权
    Apparatus for determining the phase difference between the rolling oscillation of a ship and a liquid contained in a stabilizing tank 失效
    用于确定船的滚动振荡与容纳在稳定罐中的液体之间的相位差的装置

    公开(公告)号：US3968353A

    公开(公告)日：1976-07-06

    申请号：US519677

    申请日：1974-10-31

    申请人： Herbert Kuller

    发明人： Herbert Kuller

    IPC分类号： B63B39/03 ,  G01R25/00 ,  G06G7/70 ,  G06G7/18

    CPC分类号： B63B39/03 ,  G01R25/00 ,  G06G7/70

    摘要： The measured rolling rate of a ship and a measured liquid level difference in a liquid contained in a stabilizing tank are supplied to frequency dependent members having identical frequency response to obtain a derived roll angle and derived level difference after which a circuit is provided to measure the phase difference between the quantities developed and to develop an output analog voltage representing the difference between a desired relationship between the phases of the two and the actual phase relationship.

    摘要翻译： 将测量的滚动速率和包含在稳定罐中的液体的测量液位差提供给具有相同频率响应的频率相关构件，以获得导出的侧倾角和导出的水平差，之后提供电路以测量 所产生的量之间的相位差，并且产生表示两者的相位之间的期望关系与实际相位关系之间的差的输出模拟电压。

    Sailing computer
    9.
    发明授权
    Sailing computer 失效
    救生计算机

    公开(公告)号：US3814910A

    公开(公告)日：1974-06-04

    申请号：US27736372

    申请日：1972-08-02

    申请人： COMPUTER EQUIPMENT CORP

    发明人： PALMIERI F ,  PETTINGELL J

    IPC分类号： G05D1/02 ,  G06G7/70 ,  G06G7/78

    CPC分类号： G05D1/0206 ,  G06G7/70

    摘要： A computer and a method for sailing a boat to windward to obtain maximum velocity made good. A solution algorithm permitting linear relations and a single multiplier in computing velocity made good, with apparent wind speed and angle and boat speed as the data sources.

    摘要翻译： 一种计算机和一种帆船上风以获得最大速度的方法是好的。 算法允许线性关系的解算法和单个乘法运算速度较好，具有明显的风速和角速度以及船速作为数据源。