航天标准化2024,Issue(3) :19-23.

兼容多体制标准的通用化遥控单元设计

Design of a Universal Remote Control Unit Compatible with Multiple System Standards

林型勇 季彦芳 黄才 展鹏飞 黄艳军
航天标准化2024,Issue(3) :19-23.

兼容多体制标准的通用化遥控单元设计

Design of a Universal Remote Control Unit Compatible with Multiple System Standards

林型勇 1季彦芳 1黄才 2展鹏飞 1黄艳军1
扫码查看

作者信息

  • 1. 上海航天电子技术研究所,上海,201109
  • 2. 北京空间飞行器总体设计部,北京,100094
  • 折叠

摘要

我国目前空间航天器采用的遥控体制存在多样化的情况,既有传统的脉冲编码调制(PCM)遥控体制,也有空间数据系统咨询委员会(CCSDS)遥控体制,以及高级在轨系统(AOS)标准协议.对于遥控单元,其实现通用化设计难度很大,一般都采用定制的设计方案.多航天器组合运行和组网式航天器的信息交互,对遥控单元的多体制兼容和通用化设计提出了更高的要求.文章根据多体制需求,采用多通道遥控单元的设计方案,结合通用化需求,实施遥控单元的通用化设计,可匹配目前空间航天器的遥控需求.

Abstract

At present,there is a diversity of remote control systems adopted by space vehicles in China.There are traditional PCM remote control systems,CCSDS remote control systems,as well as AOS systems.For the remote control units,it is very difficult to achieve a universal design,and customized design schemes are generally adopted.With the subsequent operation of multiple spacecraft combinations and the information interaction of networked spacecraft,higher requirements have been put forward for the multiple system compatibility and universal design of remote control units.According to the requirements of multiple systems,a design scheme of multi-channel remote control units is adopted.Combined with the universalization requirements,a universal design scheme for remote control units is implemented.This universal multi-channel remote control unit design scheme is more in line with the current remote control requirements of space vehicles.

关键词

遥控单元设计/多体制兼容/通用化/多航天器组网

Key words

remote control unit design/multiple system compatibility/universalization/networking of multiple spacecraft

引用本文复制引用

出版年

2024
航天标准化
中国航天标准化研究所

航天标准化

影响因子:0.174
ISSN:1009-234X
段落导航相关论文