|Table of Contents|

Design of WinCE-based real-time control software for rocket engine test(PDF)

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

Issue:
2011年05期
Page:
74-77
Research Field:
测控与试验
Publishing date:

Info

Title:
Design of WinCE-based real-time control software for rocket engine test
Author(s):
XU Guang-zhu WU Jin-feng
Xi’an Aerospace Propulsion Test Technique Institute, Xi’an 710100, China
Keywords:
time slice address space control logic callback function
PACS:
V416-34
DOI:
-
Abstract:
The concept and the design method of the real-time control under the WinCE operation system is described in this paper by the analysis of the WinCE operation system and its timer. The multimedia timer and the peripheral hardwares are employed in the design. The design and application of the real-time time sequence control in the pressurization and the close-cycle control system of the liquid rocket engine are introduced. The application prospect of the real-time control software design framework based on the multimedia timer is elaborated.

References:

[1]BEVERIDGE Jim, WIEN Robert. Win32多线程程序设计[M]. 武汉: 华中科技大学出版社, 2002.
[2]傅曦, 齐宇. 嵌入式系统Windows CE开发技巧与实例[M].北京: 化学工业出版社, 2004.
[3]孙鑫, 余安萍. VC++ 深入详解[M]. 北京: 电子工业出版社, 2006.
[4]RICHTER Jetfrey. Windows核心编程[M]. 5版. 北京: 清华大学出版社, 2008.

Memo

Memo:
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