航天推进技术研究院主办
[1]蒋瑜.姿控发动机试验阀门电流信号采集系统设计[J].火箭推进,2006,32(06):56-59.
Jiang Yu.Valve current signal acquisition system design for liquid attitude control rocket engine test[J].Journal of Rocket Propulsion,2006,32(06):56-59.
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Jiang Yu.Valve current signal acquisition system design for liquid attitude control rocket engine test[J].Journal of Rocket Propulsion,2006,32(06):56-59.
姿控发动机试验阀门电流信号采集系统设计
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
32
期数:
2006年06期
页码:
56-59
栏目:
出版日期:
2006-12-29
- Title:
- Valve current signal acquisition system design for liquid attitude control rocket engine test
- 分类号:
- V463
- 文献标志码:
- A
- 摘要:
- 介绍了液体火箭姿控发动机阀门电流信号采集系统的设计要点、研制方法与主要开发过程。较详细阐述了高速数据采集系统应用软件开发及系统集成后的调试方法。该采集系统实现了多路液体火箭姿控发动机试车阀门电流信号的数字化测量。
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更新日期/Last Update:
1900-01-01