Plug-and-play Fast-assembling Satellite Control System

被引：0

作者：

Yuan Dehu ^{[1
,2
]}

He Liang ^{[1
,2
]}

Lu Shan ^{[1
,2
]}

Han Fei ^{[1
,2
]}

Chen Shaohua ^{[1
,2
]}

Zhan Pengyu ^{[1
,2
]}

Sun Lujun ^{[1
,2
]}

Hu Kun ^{[1
,2
]}

Li Baohua ^{[3
]}

机构：

[1] Shanghai Inst Spaceflight Control Technol, Shanghai 200233, Peoples R China

[2] Shanghai Key Lab Airspace Intelligent Control Tec, Shanghai 200233, Peoples R China

[3] Harbin Inst Technol, Harbin 150001, Peoples R China

来源：

2013 32ND CHINESE CONTROL CONFERENCE (CCC) | 2013年

关键词：

Plug and Play; Fast Assembling; Satellite Control System;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The design scheme of a kind of plug-and-play fast-assembling satellite control system was proposed in this paper. The overall architecture of the system was introduced. The on-board computer simulator, the plug-and-play modular and the host computer software were designed respectively. And the plug-and-play time series of satellite control system devices was also described. The proposed plug-and-play satellite scheme can extremely reduce the time of coordination, development and integrated test, cut down the cost of satellite development, and enhance the reliability of spacecraft, so as to lay a good technology foundation for the development of micro-nano spacecraft and operationally responsive spacecraft.

引用

页码：7326 / 7329

页数：4