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[1]顾大陆,曾维亮,雷小飞,等.Bang-Bang阀调节的开关型贮供系统压力控制特性[J].火箭推进,2023,49(02):74-82.
 GU Dalu,ZENG Weiliang,LEI Xiaofei,et al.Pressure control characteristics of switch-type storage and supply system regulated by Bang-Bang valve[J].Journal of Rocket Propulsion,2023,49(02):74-82.
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Bang-Bang阀调节的开关型贮供系统压力控制特性

参考文献/References:

[1] 官长斌,沈岩,魏延明,等.面向空间电推力器的氙气供给系统发展综述及展望[J].宇航学报,2020,41(3):251-261.
[2] 胡竟,张天平,杨福全,等.电推力器气体比例流量控制技术的展望[J].真空与低温,2017,23(1):13-19.
[3] 谈萍,庞光庆,汤慧萍,等.霍尔电推进系统中的微流量控制器[J].功能材料,2010,41(S3):385-387.
[4] COREY R L,PIDGEON D J.Electric propulsion at space systems/loral[C]//31st International Electric Propulsion Conference.Ann Arbor,MI:University of Michigan,2009.
[5] VAN DER LIST M,VAN PUT P,YUCE V,et al.Next generation electrical propulsion feed systems and spin-off micro-propulsion components[C]//42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Reston,Virigina:AIAA,2006.
[6] FISHER J,WILSON A,KING D,et al.The development and qualification of a 4.5 kW Hall thruster propulsion system for GEO satellite applications[C]//27th International Electric Propulsion Conference.Pasadena,USA:[s.n.],2001.
[7] BARBARITS J.Xenon feed system development[C]//39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Reston,Virigina:AIAA,2003.
[8] DANKANICH J,CARDIN J,DIEN A,et al.Advanced xenon feed system(AXFS)development and hot-fire texting[C]//45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Reston,Virigina:AIAA,2009.
[9] AADLAND R,WILSON F,SCHWAB R,et al.Xenon propellant management system for 40 cm next generation ion thruster[C]//39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Reston,Virigina:AIAA,2003.
[10] 汪旭东,李国岫,陈君,等.压电比例阀调节的氙气微推进系统流量特性仿真研究[J].推进技术,2019,40(12):2867-2873.
[11] GANAPATHI G,ENGELBRECHT C.Post-launch performance characterization of the xenon feed system on deep space one[C]//35th Joint Propulsion Conference and Exhibit.Reston,Virigina:AIAA,1999.
[12] 乔彩霞,康小录,邱刚,等.SJ-9A卫星霍尔电推进系统方案及飞行试验情况[C]//2014电力电子与航天技术高峰论坛.深圳:中国电工技术学会,2014.
[13] 蒲光荣,单磊,赵晓慧,等.泵压式多次起动发动机起动过程仿真研究[J].火箭推进,2019,45(5):17-24.
PU G R,SHAN L,ZHAO X H,et al.Simulation study on start-up processes of a multi-startup turbopump-fed rocket engine[J].Journal of Rocket Propulsion,2019,45(5):17-24.
[14] KOPPEL C,MARCHANDISE F,ESTUBLIER D.Robust pressure regulation system for the SMART-1 electric propulsion sub-system[C]//40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Reston,Virigina:AIAA,2004.
[15] 贾光政,王宣银,刘昊,等.高压气动体积减压系统的Bang-Bang控制研究[J].液压与气动,2004(5):38-40.
[16] 贾光政,王宣银,吴根茂.高压气动容积减压系统研制[J].液压与气动,2003(8):14-16.
[17] 苟浩亮,潘海林.电推进系统压力调节单元的建模和分析[J].空间控制技术与应用,2008,34(5):49-52.
[18] 胡彬.基于Bang-Bang与PID控制的重型汽车ABS仿真研究与爆胎分析[D].石家庄:石家庄铁道大学,2014.
[19] 李明骏.集成Bang-Bang控制与常规控制的变工况控制:以电加热装置温度控制为例[D].北京:中国石油大学(北京),2016.
[20] 王宝龄.电磁电器设计基础[M].修订本.北京:国防工业出版社,1989.
[21] 袁洪滨,张民庆,孙彦堂.基于AMESim的直动式电磁阀动态仿真研究[J].火箭推进,2011,37(5):30-35.
YUAN H B,ZHANG M Q,SUN Y T.AMESim-based simulation analysis of dynamic characteristics of direct-acting solenoid valve[J].Journal of Rocket Propulsion,2011,37(5):30-35.
[22] 徐登伟,尤裕荣,袁洪滨,等.基于AMESim的先导膜片式电磁阀动态特性仿真[J].火箭推进,2017,43(4):41-45.
XU D W,YOU Y R,YUAN H B,et al.AMESim-based simulation analysis on dynamic characteristics of pilot-operated diaphragm solenoid valve[J].Journal of Rocket Propulsion,2017,43(4):41-45.

备注/Memo

收稿日期:2021-10-19; 修回日期:2021-11-26
基金项目:国家联合基金(U1737212)
作者简介:顾大陆(1997—),男,硕士,研究领域为火箭发动机阀门。

更新日期/Last Update: 1900-01-01