航天推进技术研究院主办
[1]许广柱,吴锦凤.基于WinCE的发动机试验实时控制软件设计[J].火箭推进,2011,37(05):74-77.
XU Guang-zhu,WU Jin-feng.Design of WinCE-based real-time control software for rocket engine test[J].Journal of Rocket Propulsion,2011,37(05):74-77.
点击复制
XU Guang-zhu,WU Jin-feng.Design of WinCE-based real-time control software for rocket engine test[J].Journal of Rocket Propulsion,2011,37(05):74-77.
基于WinCE的发动机试验实时控制软件设计
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
37
期数:
2011年05期
页码:
74-77
栏目:
测控与试验
出版日期:
2011-10-15
- Title:
- Design of WinCE-based real-time control software for rocket engine test
- 文章编号:
- 1672-9374(2011)05-0074-05
- Keywords:
- time slice; address space; control logic; callback function
- 分类号:
- V416-34
- 文献标志码:
- A
- 摘要:
- 通过对WinCE操作系统线程、进程和定时器的分析，采用多媒体定时器和外围硬件配合的方式，结合XXX液体火箭发动机试车台增压/闭环控制系统实时时序控制的设计和应用，系统论述了在WinCE操作系统下，实时控制的实现原理和设计方法，并阐述了基于多媒体定时器实时控制软件设计框架的应用前景。
- 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.
参考文献/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.
备注/Memo
收稿日期：2010-12-02；修回日期：2011-03-06
作者简介：许广柱（1975—），男，工程师，研究领域为液体火箭发动机试验系统测控技术
更新日期/Last Update:
1900-01-01