Deployable antenna
    41.
    发明公开
    Deployable antenna 有权
    Entfaltbare天线

    公开(公告)号:EP2482378A1

    公开(公告)日:2012-08-01

    申请号:EP12152827.7

    申请日:2012-01-27

    IPC分类号: H01Q1/28 H01Q15/16

    CPC分类号: H01Q15/161 H01Q1/288

    摘要: A deployable antenna which has a larger aperture diameter by four-side links provided in at least three stages and which includes: six deployment link mechanisms (20) arranged radially from a central shaft so as to support an outer edge portion of a flexible reflector mirror surface; and one deployment driving mechanism (30) arranged at a lower portion of a center of arrangement of the six deployment link mechanisms, for unfolding the six deployment link mechanisms. Each of the six deployment link mechanisms includes a first four-side link (5), a second four-side link (6), and a third four-side link (7) arranged in an order from a position of the central shaft, around which the six deployment link mechanisms are arranged, toward an outer side of the each of the six deployment link mechanisms so that the each of the six deployment link mechanisms is structured to be foldable in three stages.

    摘要翻译: 一种可展开的天线,其具有通过设置在至少三个级中的四侧链节具有较大孔径的直径,并且包括:从中心轴径向布置的六个展开连杆机构(20),以支撑柔性反射镜的外缘部分 表面; 和一个部署驱动机构(30),其布置在六个部署链接机构的排列中心的下部,用于展开六个部署链接机构。 六个展开连杆机构中的每一个包括从中心轴的位置起依次布置的第一四侧连杆(5),第二四侧连杆(6)和第三四侧连杆(7) 所述六个部署链接机构围绕所述六个部署链接机构排列,朝向所述六个部署链接机构中的每一个的外侧,使得所述六个部署链接机构中的每一个被构造成三级可折叠。

    IMAGE PICKUP DEVICE AND METHOD OF ARRANGING IMAGE PICKUP ELEMENT
    42.
    发明公开
    IMAGE PICKUP DEVICE AND METHOD OF ARRANGING IMAGE PICKUP ELEMENT 审中-公开
    BILDAUFNAHMEVORRICHTUNG UND VERFAHREN ZUR ANORDNUNG VON BILDAUFNAHMEELEMENTEN

    公开(公告)号:EP2437298A1

    公开(公告)日:2012-04-04

    申请号:EP10780411.4

    申请日:2010-05-12

    摘要: An image pickup apparatus is provided with: an optical system including a lens or a reflecting mirror; an image pickup device having a light-receiving surface on which light rays from the optical system are focused and a plurality of light-receiving pixels which generate charges on the light-receiving surface by the light rays; a bias voltage generation unit which supplies power to the image pickup device; a signal processing unit which processes a signal output from the image pickup device and outputs the processed signal as image data; and a control unit which inputs into the image pickup device a driving clock that controls transmission of the charges generate in the light-receiving pixels of the image pickup device. The image pickup device is bent so that distortion aberration present in the optical system is eliminated.

    摘要翻译: 图像拾取装置具有:包括透镜或反射镜的光学系统; 具有聚光来自光学系统的光线的受光面的多个摄像元件和在受光面上通过光线产生电荷的多个受光像素; 向图像拾取装置供电的偏置电压产生单元; 信号处理单元,处理从图像拾取装置输出的信号,并将处理后的信号作为图像数据输出; 以及控制单元,其向图像拾取装置输入控制在图像拾取装置的光接收像素中产生的电荷的传输的驱动时钟。 弯曲图像拾取装置,从而消除光学系统中存在的畸变像差。

    Data/strobe encoding scheme circuit and data/strobe encoding method
    44.
    发明公开
    Data/strobe encoding scheme circuit and data/strobe encoding method 有权
    图表数据库/ Impulskodierung und Verfahren zur Daten- / Impulskodierung

    公开(公告)号:EP1919120A1

    公开(公告)日:2008-05-07

    申请号:EP08001798.1

    申请日:2007-03-30

    IPC分类号: H04L7/02 G06F13/42 G11C7/22

    摘要: In a data/strobe encoding scheme circuit in which data and a strobe signal are transmitted through different lines, changes respectively in the data and the strobe signal are employed as clock signals for a latching operation, and the data is transmitted to a succeeding-stage circuit operating on a second clock signal. The circuit latches predetermined data by an FF circuit and passes a data pair including a signal indicating that the data has been latched and held therein as well as the latched data to the succeeding-stage circuit, activates, if assertion of a signal indicating reception of the data is received from the succeeding-stage circuit, again the FF circuit which has latched the data and has entered a stop state, and receives new data. There is provided a data/strobe encoding scheme circuit and a data/strobe encoding method, it is possible to implement a data/strobe encoding scheme circuit and a data/strobe encoding method capable of realizing a low-cost data/strobe encoding scheme which is independent of LSI device characteristics and which can be easily designed.

    摘要翻译: 在通过不同的行发送数据和选通信号的数据/选通编码方案电路中,数据和选通信号分别改变为用于锁存操作的时钟信号,并且数据被发送到后级 电路工作在第二个时钟信号上。 电路通过FF电路锁存预定数据,并将包括表示数据被锁存并保持在其中的信号以及锁存数据的数据对传送到后级电路,如果断言指示接收到 数据从后级电路再次接收到已经锁存数据并已进入停止状态并接收新数据的FF电路。 提供了数据/选通编码方案电路和数据/选通编码方法,可以实现能够实现低成本数据/选通编码方案的数据/选通编码方案电路和数据/选通编码方法, 独立于LSI器件特性,可以方便设计。

    Communication terminal, position notification method, and communication system
    45.
    发明公开

    公开(公告)号:EP1788826A1

    公开(公告)日:2007-05-23

    申请号:EP06123978.6

    申请日:2006-11-14

    发明人: Mine, Masaya

    IPC分类号: H04Q7/22

    CPC分类号: H04W4/02 H04W12/06 H04W12/08

    摘要: A communication terminal which communicates with a communication device includes a position detecting section which detects a current position of the communication terminal, and a control section which automatically notifies the communication device of the current position obtained from the position detecting section, in response to an instruction from the communication device.

    摘要翻译: 与通信装置通信的通信终端包括:位置检测部,其检测通信终端的当前位置;以及控制部,其响应于指示,自动地向通信装置通知从位置检测部获得的当前位置 从通信设备。

    Method of injecting plurality of spacecrafts into different orbits individually
    47.
    发明公开
    Method of injecting plurality of spacecrafts into different orbits individually 有权
    一种用于个人方法充电上不同的轨道的多个航天器的

    公开(公告)号:EP1679259A2

    公开(公告)日:2006-07-12

    申请号:EP06000209.4

    申请日:2006-01-05

    IPC分类号: B64G1/00 B64G1/24 B64G1/10

    摘要: Disclosed is a method for injecting a plurality of spacecrafts into different circum-earth or interplanetary orbits individually in a single launch. A plurality of spacecrafts coupled to an assist module are injected into an interplanetary orbit having a periodicity synchronous with the earth's revolution period. Then, in a maneuver for allowing the assist module to re-counter with and pass near to the earth (Earth swing-by), the assist module appropriately performs an orbital change maneuver and a separation maneuver for each of the spacecrafts in a sequential order. Through these maneuvers, a closest-approach point to the earth is changed for each of the spacecrafts so as to drastically change a subsequent orbital element for each of the spacecrafts. The assist module takes a sufficient time to determine a target orbit for each of the spacecrafts with a high degree of accuracy until a half month to several days before a closest-approach time in the Earth swing-by. Based on the determined orbit, the assist module makes an orbit correction of about several m/sec in a sequential order, and then separates the spacecrafts therefrom in a sequential order. In this process, an inertia navigation is performed based on an accelerometer mounted in the assist module and information about attitude.

    摘要翻译: 公开了一种用于在单独的单个发射注入航天器到不同circum类或星际轨道的多个方法。 耦合到辅助模块的航天器的多个被注入到在星际轨道具有与地球旋转​​周期的周期性同步。 然后,在用于允许所述辅助模块重新计数器,具有和近传递到大地(地摆动通过),辅助模块适当地执行在轨道变更操纵和按顺序的分离操纵每个航天器的机动 , 通过合成操纵,一个最近的方法点到大地改变每个航天器,以便显着地改变每个飞船的后续轨道元件。 该辅助模块需要足够的时间来确定我的每一个具有高精确度的航天器的目标轨道,直到半个月至数天在地球摇摆通过最近一次的办法了。 基于该确定的轨道开采,辅助模块使得入轨校正大约几米/秒以连续的顺序,然后从那里以连续的顺序分离空间工艺品。 在这个过程中,惯性导航是基于安装的辅助模块和大约姿态信息的加速度进行。