基于力位协同控制的航天器多路射频频谱监测系统设计

目前设计的航天器多路射频频谱监测系统采样间隔时间过长,导致监测结果与实际结果相差较大;为了解决上述问题,基于力位协同控制设计了一种新的航天器多路射频频谱监测系统,设计该监测系统的硬件和软件;在频谱分析仪的使用界面上,具有大量的射频信号控制命令,其中包含部分接口命令,通过该接口命令监测和控制频谱分析仪;单片机自带控制器,可协助系统的控制单元控制频谱;控制单元内的驱动接口电路其核心为76JG632芯片,主要对单片机内的各种接口进行供电;通过多路射频信号频谱切换、多路射频信号频谱显示、射频信号频谱监测实现软件流程;实验结果表明,所设计系统扫频和随机扫频采样的时间间隔分别为30 s和50 s,保证监测结果与实际结果吻合.

Design of Spacecraft Multi-channel RF Spectrum Monitoring System Based on Force Position Cooperative Control

At present, the sampling interval of the spacecraft multichannel RF spectrum monitoring system is too long, which results in a large difference between the monitoring results and the actual results. In order to solve these problems, a new spacecraft multi-channel radio frequency spectrum monitoring system based on force position cooperative control was designed, and the hardware and software of the monitoring system were designed. In the use interface of the spectrum analyzer, there are a large number of RF signal control commands, including some interface commands, through which the spectrum analyzer is monitored and controlled. MCU comes with a controller to assist the control unit of the system to control the spectrum; The core of the drive interface circuit in the control unit is 76JG632 chip, which mainly supplies power to various interfaces in the microcontroller. Through the multi-channel RF signal spectrum switching, multi-channel RF signal spectrum display, RF signal spectrum monitoring to achieve the software flow. The experimental results show that the spacecraft multi-channel radio frequency spectrum monitoring system based on force position cooperative control can effectively shorten the sampling interval time and ensure the monitoring results are consistent with the actual results.