|Table of Contents|

Software structure and design of LOX／kerosene engine test control system(PDF)

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

Issue:
2009年02期
Page:
46-53
Research Field:
测控与试验
Publishing date:

Info

Title:
Software structure and design of LOX／kerosene engine test control system
Author(s):
Li Congling
Xi"an Aerospace Propulsion Test Technique Institute，Xi'an 710100，China
Keywords:
liquid propellant rocket engine; test system; software design
PACS:
V434
DOI:
-
Abstract:
Software structure and design concept of the control system for the newly built rocket engine test stand are presented．The system applies the PXIbus，the modular instrument，LabVIEW DSC and LabVlEW RT，and realizes the function of sequential control，pressure regulating control， signal dynamic detection and dynamic display of test process under muhiconditions of rocket engine ground tests．The new system is characterized by high reliability and safety，real time，easy operation and maintenance，better visualization．

References:

[l]张辉，郭立．液氧／煤油发动机摇摆测控系统技术要求与 实现[J]．火箭推进，2007，33(1)：49—55．
[2]蒋慰孙，俞金寿．过程控制工程[M]．北京：中国石化出版 社．1998．
[3]王志武．基于虚拟仪器技术的信号处理与故障检测系统 [J]．火箭推进，2007，33(4)：52-56．
[4]王顺晃，舒迪前．智能控制系统及其应用[M]．北京：机械 工业出版社．2005．

Memo

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Last Update: 1900-01-01