Three dimensional balance assembly
    1.
    发明申请
    Three dimensional balance assembly 失效
    三维平衡组合

    公开(公告)号:US20060058962A1

    公开(公告)日:2006-03-16

    申请号:US11004529

    申请日:2004-12-03

    CPC classification number: G01C21/16

    Abstract: A three-dimensional balance assembly is provided. The assembly includes a center shaft, two or more eccentric weighted shafts encompassing the center shaft and a first and a second locking mechanism that lock each weighted shaft into any rotational location. Each eccentric weighted shaft includes at least one eccentric weight. The two or more eccentric weighted shafts are independently rotatable around the center shaft to balance the assembly in two dimensions. The center shaft includes a first and a second bore extending inwardly from each end of the center shaft or a single bore all the way through the shaft. The first and second bores are adapted to receive and secure one or more axial weights and balance the assembly in a third dimension.

    Abstract translation: 提供三维平衡组件。 组件包括中心轴,包围中心轴的两个或多个偏心重心轴以及将每个加重轴锁定到任何旋转位置的第一和第二锁定机构。 每个偏心重心轴包括至少一个偏心重物。 两个或更多个偏心重量轴可独立地围绕中心轴旋转,以在两个维度上平衡组件。 中心轴包括从中心轴的每个端部向内延伸的第一和第二孔,或者一直穿过轴的单个孔。 第一和第二孔适于接收和固定一个或多个轴向重物并在第三维度上平衡组件。

    RF wireless communication for deeply embedded aerospace systems
    2.
    发明申请
    RF wireless communication for deeply embedded aerospace systems 有权
    RF嵌入式航空航天系统的射频无线通信

    公开(公告)号:US20060058960A1

    公开(公告)日:2006-03-16

    申请号:US11004177

    申请日:2004-12-03

    CPC classification number: G01C21/16 G08C17/02

    Abstract: A wireless communication interface for inertial measurement unit is disclosed. One or more instrumentation sensors, a processor, a wireless radio frequency transceiver with an antenna, and a power source are sealed within an inertial sensor assembly. The processor is adapted to receive output signals from the instrumentation sensors and to convert the output signals into a stream of digital data packets. A radio frequency transceiver is coupled to the processor and adapted to wirelessly communicate the stream of digital data packets through the antenna. In one embodiment, the radio frequency transceiver is further adapted to wirelessly receive a stream of digital data packets through the antenna and communicate the received digital data packets to the processor.

    Abstract translation: 公开了一种用于惯性测量单元的无线通信接口。 一个或多个仪表传感器,处理器,具有天线的无线射频收发器和电源被密封在惯性传感器组件内。 处理器适于接收来自仪器传感器的输出信号,并将输出信号转换成数字数据包流。 射频收发器耦合到处理器并且适于通过天线无线地传送数字数据分组流。 在一个实施例中,射频收发器还适于通过天线无线地接收数字数据分组流,并将接收的数字数据分组传送到处理器。

    Generalized inertial measurement error reduction through multiple axis rotation during flight
    3.
    发明申请
    Generalized inertial measurement error reduction through multiple axis rotation during flight 有权
    飞行过程中通过多轴旋转的广义惯性测量误差减少

    公开(公告)号:US20060053887A1

    公开(公告)日:2006-03-16

    申请号:US11004517

    申请日:2004-12-03

    Applicant: Robert Fall

    Inventor: Robert Fall

    CPC classification number: G01C21/165 B64G1/36 G01C19/34

    Abstract: An inertial measurement unit is provided. The inertial measurement unit comprises two rotational axes, wherein a first of the two rotational axes is aligned nominally along a thrust axis and a second of the two rotational axes is aligned substantially perpendicular to a plane formed by a local gravity vector and a thrust vector, and one or more sensors which rotate about the second rotational axis.

    Abstract translation: 提供惯性测量单元。 惯性测量单元包括两个旋转轴,其中两个旋转轴中的第一个沿着推力轴线标称对准,并且两个旋转轴中的第二个旋转轴基本上垂直于由局部重力向量和推力矢量形成的平面排列, 以及围绕第二旋转轴线旋转的一个或多个传感器。

    SYSTEMS AND METHODS FOR IMPROVED INERTIAL NAVIGATION
    4.
    发明申请
    SYSTEMS AND METHODS FOR IMPROVED INERTIAL NAVIGATION 失效
    改进的惯导系统和方法

    公开(公告)号:US20070271037A1

    公开(公告)日:2007-11-22

    申请号:US11383895

    申请日:2006-05-17

    CPC classification number: G01S19/47

    Abstract: A method for producing inertial measurement data is provided. The method comprises receiving raw inertial measurement data from one or more inertial sensors; receiving raw position data based on signals from a global navigation satellite system; processing the raw inertial measurement data and the raw position data with a filter to generate state variable estimates; and calculating enhanced inertial measurement data based on the raw inertial measurement data and the state variable estimates from the filter.

    Abstract translation: 提供了一种制造惯性测量数据的方法。 该方法包括从一个或多个惯性传感器接收原始惯性测量数据; 基于来自全球导航卫星系统的信号接收原始位置数据; 用滤波器处理原始惯性测量数据和原始位置数据以生成状态变量估计; 并且基于原始惯性测量数据和来自过滤器的状态变量估计来计算增强的惯性测量数据。

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