|Table of Contents|

Pressure contr01 system based on LabView for 1iquid oxyge/kerosene Vessel(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2008年06期
Page:
40-44
Research Field:
测控与试验
Publishing date:

Info

Title:
Pressure contr01 system based on LabView for 1iquid oxyge/kerosene Vessel
Author(s):
Li Dangke; Zhang Hui
Xi，an Aemspace Propulsion Test Technique Institute，Xi7an 710100，China
Keywords:
Labview; control of Vessel pressure; real—time system
PACS:
V434.3
DOI:
-
Abstract:
The design requirements and system composition of propellant vessel pressure control system for liquid rocket engine ground test and the software deVelopment based on Labview under real time system were introduced in this paper．The principle of the vessel pressure contml system， technolog)，characteristics and the system fhmework were described in detail．Centralized control of multi—channel signals was obtained and was proved successfhl by ground tests．

References:

[l]张海藩．软件T．程导论[M]．北京：清华大学出版社，2004．
[2]Jean J Labmsse．嵌入式实时操作系统[M]．北京：北京航 空航天大学出版社，2006．
[3]王平．计算机控制系统[M]．北京：高等教育出版社，2004．
[4]杨乐平．Labview高级程序设计[M]．北京：清华大学出版 社。2004．
[5]National Instrument．Rea--time OS User，s Manua玎MI 2()04．
[6]李伟民．液氧／煤油发动机试验系统[J]．火箭推进，2005，3l (6l：50—56，

Memo

Memo:
-
Last Update: 1900-01-01