Method for processing a radar echo signal
    2.
    发明授权
    Method for processing a radar echo signal 有权
    雷达回波信号处理方法

    公开(公告)号:US07978125B2

    公开(公告)日:2011-07-12

    申请号:US12564788

    申请日:2009-09-22

    申请人: Nicola Battisti

    发明人: Nicola Battisti

    IPC分类号: G01S13/00 G01S13/52

    CPC分类号: G01S13/9029 G01S2013/9064

    摘要: A method to process a radar echo signal is described. The method determines the value of at least one target motion parameter by selecting from a plurality of possible test values (VR1, . . . , VRN) one value (VR) which maximizes a functional defined over the radar echo signal. The method further performs a correction of the radar echo signal based on the value (VR) which is determined by the at least one motion parameter. The functional is the time derivative of the radar echo signal or a function dependent from the derivative.

    摘要翻译: 描述了一种处理雷达回波信号的方法。 该方法通过从多个可能的测试值(VR1,...,VRN)中选择使得在雷达回波信号上定义的功能最大化的一个值(VR)来确定至少一个目标运动参数的值。 该方法还基于由至少一个运动参数确定的值(VR)进行雷达回波信号的校正。 功能是雷达回波信号的时间导数或与导数相关的函数。

    Housing-transportation-launch assembly and method
    3.
    发明授权
    Housing-transportation-launch assembly and method 有权
    住房运输发射组装和方法

    公开(公告)号:US07891281B2

    公开(公告)日:2011-02-22

    申请号:US11400017

    申请日:2006-04-07

    IPC分类号: F41F3/042

    摘要: In a ground launcher, two or more housing-transportation-launch assemblies for respective missiles are placed one on top of the other and connected releasably and interchangeably to each other; each housing-transportation-launch assembly has a respective outer casing, which in turn has longitudinal end walls breakable from inside the casing, and a deflecting body for deflecting the exhaust gas of the engine of the missile; a guide and protection assembly being interposed between the casing and the missile to guide the missile in the set launch direction, and to protect the missile against shock or vibration.

    摘要翻译: 在地面发射器中,用于各个导弹的两个或多个外壳运输发射组件一个放置在另一个的顶部上,并且彼此可释放地和互换地相连; 每个壳体运输发射组件具有相应的外壳,其又具有可从壳体内部破裂的纵向端壁和用于偏转导弹发动机的排气的偏转体; 引导和保护组件插入在外壳和导弹之间以在发射方向上引导导弹,并保护导弹免受冲击或振动。