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一种现代航天器飞行控制系统及其容错技术研究
Alternative TitleResearch on spacecraft flight control system andits fault·tolerant technique
段海滨; 于秀芬; 王道波; 北京8701信箱
Department国家863计划微波遥感技术实验室
Source Publication电光与控制
2004
Volume11Issue:3Pages:40-43
ISSN1671-637X
Language中文
Keyword航天器飞行控制系统 光纤 容错技术 tmrs
Abstract阐述了一种现代航天器飞行控制系统的组成原理及其类别,阐述了时分复用和波分复用的性能特点,进一步提出了光纤多路发送软件、接收软件的设计技术.在详尽介绍容错技术的基础上,设计了一种现代航天器飞行控制系统三余度容错技术方案.实例仿真验证表明,本文所设计的现代航天器容错系统是可行的,并具有很强的鲁棒性.
Other AbstractThis paper presented the principle and the types of current Spacecraft Fli.sht Control System (SFCS).The characteristics of Time Division Multiplex(TDM)and Wavelength Division Multiplex(WDM)were illustrated.The design of concerned software for multiplex sending an dreceiving was also yen.With the detailed introduction of fault-tolerant technique,a typical SFCS fault-tolerant technique scheme was proposed.The experimental results verified that the fault-tolerant system is feasible and has good robustness.
Funding Project中国科学院空间科学与应用研究中心
Document Type期刊论文
Identifierhttp://ir.nssc.ac.cn/handle/122/2014
Collection微波遥感部
Corresponding Author北京8701信箱
Recommended Citation
GB/T 7714
段海滨,于秀芬,王道波,等. 一种现代航天器飞行控制系统及其容错技术研究[J]. 电光与控制,2004,11(3):40-43.
APA 段海滨,于秀芬,王道波,&北京8701信箱.(2004).一种现代航天器飞行控制系统及其容错技术研究.电光与控制,11(3),40-43.
MLA 段海滨,et al."一种现代航天器飞行控制系统及其容错技术研究".电光与控制 11.3(2004):40-43.
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