Device and method for detecting an angular position of a rotating object
    51.
    发明授权
    Device and method for detecting an angular position of a rotating object 有权
    用于检测旋转物体的角位置的装置和方法

    公开(公告)号:US07369960B2

    公开(公告)日:2008-05-06

    申请号:US10703113

    申请日:2003-11-06

    Inventor: Lothar Blossfeld

    CPC classification number: G01D5/24476 G01D5/2448

    Abstract: In detecting the time at which a rotating object passes a given angular position, a value range of an angular position sensor output signal which varies relatively rapidly with angular position acts as a trip threshold that, when exceeded, indicates the object has achieved the detected angular position. A relatively rapid change as a function of angular position is determined by reference to the functional dependence of the detection signal level on the angular position of the object. Assuming the sensor signal varies sinusoidally with the object's angular position, the ranges in which the level of the sensor output signal varies rapidly with angular position lie in the vicinity of the angular positions at which the sensor output signal crosses its own mean value, the threshold value being chosen near this mean value.

    Abstract translation: 在检测旋转物体经过给定角度位置的时间时,与角位置相对快速变化的角位置传感器输出信号的值范围用作跳闸阈值,当超出时,该值范围表示物体已经实现了检测到的角 位置。 通过参考检测信号电平对物体的角位置的功能依赖性来确定作为角位置的函数的相对快速的变化。 假设传感器信号与物体的角度位置正弦变化,则传感器输出信号的电平随角度位置快速变化的范围位于传感器输出信号穿过其自身平均值的角位置附近,阈值 在该平均值附近选择值。

    Navigational indicating system for rotary wing aircraft
    52.
    发明授权
    Navigational indicating system for rotary wing aircraft 有权
    旋翼飞机导航指示系统

    公开(公告)号:US07324016B1

    公开(公告)日:2008-01-29

    申请号:US11288070

    申请日:2005-11-22

    Inventor: Judah H. Milgram

    CPC classification number: B64C27/46 B64C27/023 B64D47/06 B64D2203/00

    Abstract: Red, green and white colored lights are emitted from navigation orientation indicating light emitting devices mounted within a helicopter rotor blade near its tip. The light emissions from such devices are under control to respectively indicate passage of the rotor blade through limited arcuate portions of the travel path of the rotor blade end tip. Operational control over the light emitting devices is effected by data processing of outputs from air-speed responsive sensors on the blade end tip.

    Abstract translation: 导航方向发出红色,绿色和白色的指示灯,指示安装在其尖端附近的直升机转子叶片内的发光装置。 来自这种装置的光发射受到控制,以分别指示转子叶片通过转子叶片末端的行进路径的有限弓形部分的通过。 对发光装置的操作控制是通过对来自叶片末端的空速响应传感器的输出的数据处理来实现的。

    Method and apparatus for generating magnetic field map and method and apparatus for checking pose of mobile body using the magnetic field map
    53.
    发明授权
    Method and apparatus for generating magnetic field map and method and apparatus for checking pose of mobile body using the magnetic field map 有权
    用于产生磁场图的方法和装置以及使用磁场图检查移动体姿势的方法和装置

    公开(公告)号:US07302345B2

    公开(公告)日:2007-11-27

    申请号:US11035742

    申请日:2005-01-18

    CPC classification number: G01R33/10 G05D1/0259 G05D1/0274

    Abstract: Provided is a method of generating a magnetic field map including obtaining magnetic field information, the magnetic field information being information on a magnetic field affecting a mobile body, for each position of the mobile body, and building a magnetic field map based on the magnetic field information for each position of the mobile body. The pose of a mobile body can be statistically checked by the probability obtained using the difference between the magnetic field information observed from the magnetic field map and the actually measured magnetic field information. Although the pose of the mobile body is estimated using a camera that is sensitive to an illumination state where the mobile body is placed, the pose of the mobile body can be relatively accurately checked using the magnetic field map obtained in a situation regardless of illumination, with being less affected by the illumination state where the mobile body is placed. Thus, the pose of the mobile body can be checked with reliability.

    Abstract translation: 本发明提供一种生成磁场映射的方法,包括获得磁场信息,磁场信息是关于移动体的每个位置的影响移动体的磁场的信息,以及基于磁场建立磁场图 关于移动体的每个位置的信息。 可以通过使用从磁场映射观察到的磁场信息与实际测量的磁场信息之间的差异获得的概率统计地检查移动体的姿态。 虽然使用对放置移动体的照明状态敏感的照相机来估计移动体的姿态,但是可以使用在不管照明的情况下获得的磁场图来相对精确地检查移动体的姿态, 受到移动体的放置状态的影响较小。 因此,可以可靠地检查移动体的姿势。

    System for determining three dimensional position of radio transmitter
    54.
    发明申请
    System for determining three dimensional position of radio transmitter 有权
    确定无线电发射机三维位置的系统

    公开(公告)号:US20070265799A1

    公开(公告)日:2007-11-15

    申请号:US11797224

    申请日:2007-05-01

    Applicant: Kentaro Yamada

    Inventor: Kentaro Yamada

    CPC classification number: G01S5/12 G01S1/68 G06K2017/0045

    Abstract: The present invention intends to provide a method for accurately and quickly estimating a three-dimensional position of a radio transmitter. The present invention provides a method for estimating a three-dimensional position of a radio transmitter. The method includes: a step of moving a mobile object provided with a radio receiver in a workspace to a position where the radio receiver receives a radio signal from a radio transmitter, a step of storing a receiving state of the radio signal as the mobile object performs a predetermined operation when the radio receiver receives the radio signal, and a step of determining a three-dimensional position of the radio transmitter based on the receiving state.

    Abstract translation: 本发明旨在提供一种用于准确且快速地估计无线电发射机的三维位置的方法。 本发明提供一种用于估计无线电发射机的三维位置的方法。 该方法包括:将在工作空间中设置有无线电接收机的移动对象移动到无线电接收机从无线电发射机接收无线电信号的位置的步骤,存储无线电信号的接收状态作为移动对象的步骤 当无线电接收机接收无线电信号时执行预定的操作,以及基于接收状态确定无线电发射机的三维位置的步骤。

    System and method for computing reachable areas
    55.
    发明申请
    System and method for computing reachable areas 失效
    用于计算可到达区域的系统和方法

    公开(公告)号:US20070255524A1

    公开(公告)日:2007-11-01

    申请号:US11413925

    申请日:2006-04-27

    CPC classification number: F41G7/007 F41G9/00

    Abstract: The present invention relates to computing reachable areas given a first point. More specifically, the present invention relates to the computation of an intersection between a first surface and a second surface for determining a set of points that are reachable from a first point. Using the present invention, a user can determine either (1) a locus of target sites that can be struck by a ballistic projectile from a given launch site, or (2) a locus of launch sites that can be used to hit a given target site. The disclosed system and method employs graphics hardware to determine an intersection between a first surface defined by trajectory paths, and a second surface defined by terrain.

    Abstract translation: 本发明涉及计算可达到的第一点的区域。 更具体地,本发明涉及第一表面和第二表面之间的交叉点的计算,用于确定从第一点可到达的一组点。 使用本发明,用户可以确定(1)可以从给定发射场点被弹道射弹击中的目标位置的轨迹,或者(2)可用于击中给定目标的发射场所的轨迹 现场。 所公开的系统和方法使用图形硬件来确定由轨迹路径限定的第一表面和由地形限定的第二表面之间的交点。

    Method and system for personal inertial navigation measurements
    56.
    发明授权
    Method and system for personal inertial navigation measurements 有权
    个人惯性导航测量方法和系统

    公开(公告)号:US07280936B1

    公开(公告)日:2007-10-09

    申请号:US11379602

    申请日:2006-04-21

    CPC classification number: G01C21/16

    Abstract: A system (400, 500) and method (800) of personal inertial navigation measurements can include measuring (802) an angle, measuring (804) an angular velocity independent of an angle measurement, measuring (806) an angular acceleration independent of the angle measurement and independent of an angular velocity measurement, and combining (808) the angle measurement, the angular velocity measurement, and an angular acceleration to provide an angled output. The angle measurement can be measured using a compass or magnetic field, the angular velocity can be measured using a gyroscope (such as a MEMS gyroscope), and the angular acceleration measurement can be measured using an angular accelerometer (such as a molecular electronic transfer device having a magneto hydrodynamic effect device). The method can further include suppressing (810) noise caused by the angle measurement by using a sample and hold circuit (504) controlled by a higher ordered component to suppress noise from a lower ordered component.

    Abstract translation: 个人惯性导航测量的系统(400,500)和方法(800)可以包括测量(802)角度,测量(804)与角度测量无关的角速度,测量(806)与角度无关的角加速度 测量并且独立于角速度测量,并且组合(808)角度测量,角速度测量和角加速度以提供成角度的输出。 可以使用罗盘或磁场测量角度测量,可以使用陀螺仪(例如,MEMS陀螺仪)来测量角速度,并且角加速度测量可以使用角加速度计(例如分子电子转移装置 具有磁流体动力学效应装置)。 该方法还可以包括通过使用由较高阶分量控制的采样和保持电路(504)来抑制(810)由角度测量引起的噪声,以抑制来自低阶分量的噪声。

    Self-balancing, no-spin magnet compass
    57.
    发明授权
    Self-balancing, no-spin magnet compass 失效
    自平衡,无旋转磁铁罗盘

    公开(公告)号:US07194814B2

    公开(公告)日:2007-03-27

    申请号:US10851082

    申请日:2004-05-24

    CPC classification number: G01C17/18

    Abstract: A self-balancing, no-spin magnetic compass. A described embodiment includes a compass card assembly, a retainer assembly, a pivot assembly, a gimbal assembly, a cup, and a dome. The compass card assembly includes an air chamber which provides buoyancy. The retainer assembly functions with the compass card assembly to retain magnets. The pivot assembly snap-fits into the retaining assembly and contacts the compass card assembly to allow the compass card assembly to pivot about the pivot assembly. The pivot assembly also snap-fits into the gimbal assembly. The base of the pivot assembly is positioned into the cup and the entire compass is secured into the dome, that is filled with a fluid.

    Abstract translation: 自动平衡,无旋转磁罗盘。 所描述的实施例包括罗盘卡组件,保持器组件,枢轴组件,万向节组件,杯和圆顶。 罗盘卡组件包括提供浮力的空气室。 保持器组件与罗盘卡组件一起工作以保持磁体。 枢轴组件卡扣配合到保持组件中并接触罗盘卡组件,以允许罗盘卡组件围绕枢轴组件枢转。 枢轴组件也卡扣到万向节组件中。 枢轴组件的基座定位在杯中,并且整个罗盘被固定到圆顶中,其中填充有流体。

    Self-contained, non-intrusive data acquisition in ammunition
    58.
    发明申请
    Self-contained, non-intrusive data acquisition in ammunition 失效
    弹药中独立,非侵入性的数据采集

    公开(公告)号:US20070067138A1

    公开(公告)日:2007-03-22

    申请号:US11250690

    申请日:2005-09-21

    CPC classification number: F42B12/365 F41A31/00 F42B35/00

    Abstract: Various implementations are disclosed for self-contained, non-intrusive data collection in ammunition. In some implementations, a gun is loaded with a non-explosive, non-firing round of ammunition containing a data acquisition system. Such a data-collecting round of ammunition may be loaded into the gun according to the same procedures as live rounds of ammunition, and, in particular, may be loaded into a firing position immediately after a preceding live round has been fired. In this way, the data-collecting round of ammunition is able to experience temperature or other conditions that are experienced essentially identically by live rounds. After collecting related data while in the firing position, the data-collecting round may be removed from the gun, for analysis of the data for, for example, development of hot gun misfire safety procedures.

    Abstract translation: 公开了各种实施方案,用于在弹药中进行自包含的非侵入式数据收集。 在一些实施方案中,枪装有包含数据采集系统的非爆炸性,非发射弹药弹。 这样的数据收集弹药可以按照与弹药的现场循环相同的程序装载到枪中,并且特别地,可以在先前的生命周期被触发之后立即装入射击位置。 以这种方式,弹药的数据收集能够体验温度或其他通过实况相同的经验。 在点火位置收集相关数据之后,可以从枪中取出数据收集轮,以便分析数据,例如开发热枪失火安全程序。

    Method for determining the 3D coordinates of the surface of an object
    59.
    发明申请
    Method for determining the 3D coordinates of the surface of an object 有权
    用于确定物体表面的3D坐标的方法

    公开(公告)号:US20060265177A1

    公开(公告)日:2006-11-23

    申请号:US11436212

    申请日:2006-05-18

    CPC classification number: G01B11/002 G01S17/89

    Abstract: A method serves to determine the 3D coordinates of an object. The 3D coordinates of a partial surface (6) of the object are determined by a 3D measuring device (3), which includes one or more detectors (4) and whose position is determined by a tracking system. The 3D coordinates of an adjacent partial surface (7) of the object are determined by the 3D measuring device (3). The 3D coordinates of an overlap region of the adjacent partial surfaces (6, 7) are put together by a matching method. In doing so, an error function is determined and minimized iteratively. Furthermore, the error function of a detector (4) of the 3D measuring device (3) is determined.

    Abstract translation: 一种方法用于确定对象的3D坐标。 物体的部分表面(6)的3D坐标由包括一个或多个检测器(4)并且其位置由跟踪系统确定的3D测量装置(3)确定。 物体的相邻部分表面(7)的3D坐标由3D测量装置(3)确定。 通过匹配方法将相邻部分表面(6,7)的重叠区域的3D坐标放在一起。 在这样做时,迭代地确定和最小化误差函数。 此外,确定3D测量装置(3)的检测器(4)的误差函数。

    RELATIVE RANGE CAMERA CALIBRATION
    60.
    发明申请

    公开(公告)号:US20060195292A1

    公开(公告)日:2006-08-31

    申请号:US11382022

    申请日:2006-05-06

    Applicant: John Krumm

    Inventor: John Krumm

    Abstract: Method and system for measuring a relative position and orientation of range cameras using a movement of an object within a scene. In general, the method and system determine the relative pose between two cameras by measuring a path the movement of the object makes within a scene and calculating transformation parameters based on these measurements. These transformation parameters are used to determine the relative position of each camera with respect to a base camera. The system and method include other novel features, such as a data synchronization feature that uses a time offset between cameras to obtain the transformation parameters, and a technique that improves the robustness and accuracy of solving for the transformation parameters, and an interpolation process that interpolates between sampled points if there is no data at a particular instant in time.

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