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Rendezvous docking controller

机译:交会对接控制器

摘要

PURPOSE:To miniaturize a propulsion device of a space equipment by receiving the radio wave to be transmitted from a GPS satellite to a target satellite and a chaser satellite respectively, outputting the information on the present position and time, and mounting a receiving device to transmit the received information to each control means as the input information. CONSTITUTION:A chaser satellite 1 and a target satellite 2 receive the positional signal and the time signal 22 from at least four GPS satellites, and the time of the satellite is calibrated with reference to the GPS time to make the satellite time coincident with each other. The chaser satellite 1 prepares the procedures of the docking operation based on the macro command required for a series of docking operation transmitted from an earth station, and the table data to develop this macro command into the fundamental command groups with the effective time described in the satellite time, and transmits the command for the target satellite to the target satellite prior to the docking operation.
机译:目的:通过分别接收将从GPS卫星发射到目标卫星和追逐卫星的无线电波,输出有关当前位置和时间的信息,并安装接收装置以使空间设备的推进装置小型化接收到的信息作为输入信息送到每个控制装置。组成:追赶卫星1和目标卫星2从至少四个GPS卫星接收位置信号和时间信号22,并参考GPS时间对卫星时间进行校准,以使卫星时间彼此重合。跟踪卫星1根据从地球站发送的一系列对接操作所需的宏命令,准备表对接操作的程序,并利用该表数据将该宏命令发展为基本命令组,并在有效时间中进行描述。卫星时间,并在对接操作之前将目标卫星的命令发送到目标卫星。

著录项

  • 公开/公告号JP2565087B2

    专利类型

  • 公开/公告日1996-12-18

    原文格式PDF

  • 申请/专利权人 NIPPON ELECTRIC CO;

    申请/专利号JP19930152317

  • 发明设计人 MYOSHI HIROAKI;

    申请日1993-06-23

  • 分类号B64G1/64;B64G1/24;

  • 国家 JP

  • 入库时间 2022-08-22 03:28:45

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