首页> 外国专利> DEVICE FOR CONTROLLING RELATIVE POSITION(S) BY POWER MEASUREMENTS, FOR A SPACECRAFT OF A GROUP OF SPACECRAFT IN FORMATION

DEVICE FOR CONTROLLING RELATIVE POSITION(S) BY POWER MEASUREMENTS, FOR A SPACECRAFT OF A GROUP OF SPACECRAFT IN FORMATION

机译:通过功率测量控制相对位置的装置,用于形成一组空间工艺的空间工艺

摘要

A control device (D), for a spacecraft of a group of spacecraft which is intended to move according to a chosen formation, comprises i) an assembly of at least three send/receive antennas (A1-A3) installed on at least three faces of different orientations of its spacecraft and suitable for sending/receiving RF signals, ii) first measurement means (M1) responsible for determining the power of the signals received by each of the antennas (A1-A3) and for delivering power sets each associated with one of the other spacecraft of the group, iii) storage means (BD) responsible for storing cartographic data sets each representative of normalized powers of the signals received by each of the antennas (A1-A3) as a function of chosen directions of transmission, and iv) processing means (MT) responsible for comparing each power set delivered by the first measurement means (M1) with the stored cartographic data sets, so as to estimate each direction of transmission of the signals sent by the other spacecraft of the group with respect to a reference system tied to their spacecraft.
机译:用于一组航天器的航天器的控制装置(D),其旨在根据选定的构造进行移动,包括:i)至少三个安装在至少三个面上的发送/接收天线(A1-A3)的组件ii)第一测量装置(M1),负责确定每个天线(A1-A3)接收到的信号的功率,并传递与以下各项相关的功率集: iii)负责存储制图数据集的存储装置(BD),每个存储装置代表由每个天线(A1-A3)接收的信号的归一化功率,这些功率是所选择的传输方向的函数, iv)处理装置(MT),其负责将由第一测量装置(M1)传送的每个功率集与所存储的制图数据集进行比较,以便估计由另一个测量装置发送的每个信号的传输方向该小组的航天器相对于与其航天器相关的参考系统。

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