System and method for measuring physical parameters using an integrated
multisensor system
    1.
    发明授权
    System and method for measuring physical parameters using an integrated multisensor system 有权
    使用集成多传感器系统测量物理参数的系统和方法

    公开(公告)号:US6134485A

    公开(公告)日:2000-10-17

    申请号:US252584

    申请日:1999-02-18

    摘要: A system and method for analyzing physical parameters of flight data at a plurality of discrete locations about a surface of an aircraft includes a multisensor system having an array of belts. Each belt includes a plurality of interconnected belt segments including a substrate having an electrically conductive digital data bus, and at least one module having a first sensor, a second sensor and a digital signal processor, and a coating for protecting the belt segment. The first and second sensors, which are preferably formed as microelectromechanical sensors sharing a common substrate, respectively generate signals representative of a first physical parameter and a second physical parameter. The processor receives and analyzes the first and second signals to generate a third signal. The third signal is transmitted along the electrically-conductive bus to a remotely-located controller. The controller analyzes the third signal to obtain flight status information relating to the effect of the physical parameters on the flight.

    摘要翻译: 用于分析在飞行器表面周围的多个离散位置处的飞行数据的物理参数的系统和方法包括具有带阵列的多传感器系统。 每个带包括多个相互连接的带段,包括具有导电数字数据总线的衬底,以及具有第一传感器,第二传感器和数字信号处理器的至少一个模块以及用于保护带段的涂层。 优选地形成为共享公共衬底的微机电传感器的第一和第二传感器分别产生表示第一物理参数和第二物理参数的信号。 处理器接收并分析第一和第二信号以产生第三信号。 第三信号沿着导电总线传输到远程位置的控制器。 控制器分析第三信号以获得与飞行上的物理参数的影响有关的飞行状态信息。

    SYSTEM AND METHOD FOR MEASURING PARAMETERS AT AIRCRAFT LOCI
    2.
    发明申请
    SYSTEM AND METHOD FOR MEASURING PARAMETERS AT AIRCRAFT LOCI 审中-公开
    用于在飞机位置测量参数的系统和方法

    公开(公告)号:US20080228331A1

    公开(公告)日:2008-09-18

    申请号:US11686057

    申请日:2007-03-14

    IPC分类号: G06F17/00

    CPC分类号: H04Q9/00

    摘要: A system for measuring parameters at a plurality of loci associated with an aircraft includes: (a) a central unit; (b) a plurality of communicating nodes coupled with the central unit; and (c) a respective plurality of sensing units associated with each respective communicating node of the plurality of communicating nodes; at least one selected sensing unit of at least one respective plurality of sensing units being a remote sensing unit. The at least one remote sensing unit communicates wirelessly with the respective communicating node.

    摘要翻译: 用于测量与飞行器相关联的多个轨迹上的参数的系统包括:(a)中央单元; (b)与中央单元耦合的多个通信节点; 和(c)与所述多个通信节点中的每个相应通信节点相关联的相应的多个感测单元; 至少一个相应的多个感测单元的至少一个选择的感测单元是遥感单元。 所述至少一个遥感单元与相应的通信节点进行无线通信。