PDF下载 分享
[1]李雪松,康小明,张亚欧,等.基于LabVIEW的快速往复朗缪尔探针诊断系统[J].火箭推进,2014,40(01):81-84.
 LI Xue-song,KANG Xiao-ming,ZHANG Ya-ou,et al.Fast reciprocating Langmuir probe diagnostic system based on LabVIEW[J].Journal of Rocket Propulsion,2014,40(01):81-84.
点击复制

基于LabVIEW的快速往复朗缪尔探针诊断系统

参考文献/References:

[1]DUNNING J W, HAMLEY J A, JANKOVSKY R S, et al. An overview of electric propulsion activities at NASA, AIAA2004-3328[R]. USA: AIAA, 2004.
[2]一林. 电推进发展现状[J]. 国际太空, 2004 (6): 24-26.
[3]朱毅麟. 电推进的现状与展望[J]. 上海航天, 1998, 15(003): 48-53.
[4]奥切洛, 弗拉姆. 等离子体诊断[M]. 郑少白, 译. 北京: 电子工业出版社, 1944.
[5]MILNES K A, EHLERS K W , LEUNG K N, et al. A fast Langmuir probe sweeping circuit[J]. Transaction on Plas- ma Science. 1980, 8(2): 124-126.
[6]王磊, 陶梅. 精通LabVIEW8.0[M]. 北京: 电子工业出版社, 2007.
[7]乔毅, 栾矢艳, 袁爱进. 基于LabVIEW和OPC的数据通信的实现[J]. 控制工程, 2005, 12(2): 153-155.
[8]陈树学, 刘萱. LabVIEW 宝典[M]. 北京: 电子工业出版社, 2012.
[9]MITCHNER M, KRUGER C, FONTANESI M A. 400 kHz,fast-sweep Langmuir probe for measuring plasma fluctua- tions[J]. Review of Scientific Instruments, 1999, 70(6):2681-2688.
[10]HUDDLESTONE R H, LEONARD S H. Plasma diagnos- tic techniques[M]. New York: Academic Press, 1965.
[11]PRUVIS C K. Design guidelines for assessing and con- trolling spacecraft charging effect[M]. USA: Scientific and Technical Information Branch of NASA, 1984.
[12]林榕, 毛根旺. 用Langmuir探针诊断MPT羽流[J]. 固体火箭技术, 2005, 28(2): 149-152.
[13]张宝芳. 微波等离子体的静电探针测试系统的研究设计[D]. 成都: 电子科技大学, 2008.
[14]池凌飞, 林揆训, 姚若河, 等. Langumir单探针诊断射频辉光放电等离子体及其数据处理[J]. 物理学报, 2001, 50(7): 1313-1317.
[15]MAWARDI O K. Use of Langmuir probes for low-density plasma diagnostics[J]. American Journal of Physics, 1966, 34(2): 112-120.

相似文献/References:

[1]刘小杰,杜永清,张鹤平,等.基于LabVIEW与PLC的烧嘴 试验台测控系统设计[J].火箭推进,2015,41(03):108.
 LIU Xiao-jie,DU Yong-qing,ZHANG He-ping,et al.Design of measurement and control system for burner test bench based on LabVIEW and PLC[J].Journal of Rocket Propulsion,2015,41(01):108.
[2]李党科.张辉.基于Labview的液氧/煤油贮箱压力控制软件[J].火箭推进,2008,34(06):40.
 Li Dangke,Zhang Hui.Pressure contr01 system based on LabView for 1iquid oxyge/kerosene Vessel[J].Journal of Rocket Propulsion,2008,34(01):40.
[3]刘小杰,杜永清.基于LabVIEW的调节器低温动性能试验台测量系统设计[J].火箭推进,2016,42(05):110.[doi:10.3969/j.issn.1672-9374.2016.05.019]
 LIU Xiaojie,DU Yongqing.Design of LabVIEW-based measuring system for cryogenic dynamic performance test bench for regulator[J].Journal of Rocket Propulsion,2016,42(01):110.[doi:10.3969/j.issn.1672-9374.2016.05.019]

备注/Memo

收稿日期:2013-08-07;修回日期:2013-10-15 作者简介:李雪松(1988—),硕士生,研究领域为推进理论和电推进技术

更新日期/Last Update: 1900-01-01