Spacecraft disciplined reference oscillator
    2.
    发明公开
    Spacecraft disciplined reference oscillator 有权
    Dislabinierter参考振荡器fürRaumfahrzeuge

    公开(公告)号:EP0899637A1

    公开(公告)日:1999-03-03

    申请号:EP98306811.5

    申请日:1998-08-26

    IPC分类号: G04G7/02

    CPC分类号: G04G7/02 G01S19/14

    摘要: An earth orbit satellite control system which provides automatic, continuous correction of phase and frequency in order to maintain synchronization between the satellite (1) and a Global Positioning System (GPS) (2). The system achieves phase and frequency synchronization by disciplining the satellite's reference oscillator (10) by phase locking it to timing pulses received from the GPS (12). The system comprising a state machine controller (12) which cycles the disciplined oscillator (10) into both a closed-loop operation wherein the oscillator is phase-locked to the GPS timing pulses, and an open-loop operation wherein a previously stored GPS timing pulse, or commands from a ground station (3), drive oscillator phase and frequency synchronization.

    摘要翻译: 二阶数字锁相环执行卫星参考振荡器的相位锁定,以参考从GPS(2)接收的定时脉冲。 基准振荡器的相位和频率被连续和自动地校正,以便在闭环或开环操作模式之一期间保持卫星(1)和GPS之间的同步。 基于来自地面控制系统的命令来选择性地修改参考振荡器,以便分配存储在卫星上的值或从地面控制系统发送的值。 - 具有二阶数字锁相环的锁相作为锁相环专用集成电路实现。 存储在卫星上的值是接收的GPS参考定时脉冲与从参考振荡器的输出导出的内部定时脉冲之间的相位差。 对相位差进行滤波以提供将相位差降至零的控制电压调整信号。 通过对由参考振荡器输出的19.38 MHz时钟获得的时钟信号进行递减计算得到内部定时脉冲。 卫星同步系统包含独立声明。