空间太阳电池阵静电放电数值模拟研究
详细信息 查看官网全文
- 英文论文题名：Space solar cell array electrostatic discharge numerical simulation research
- 论文作者：蒙志成 ; 孙永卫 ; 原青云 ; 曹鹤飞 ; 刘浩
- 英文论文作者：MENG Zhi-cheng ; SUN Yong-wei ; YUAN Qing-yun ; CAO Hei-fei ; LIU Hao ; Institute of Electrostatic & Electromagnetic Protection ; Mechanical Engineering College
- 年：2015
- 作者机构：军械工程学院静电与电磁防护研究所;
- 论文关键词：太阳电池阵 ; 等效电路 ; 数值模拟 ; 一次放电 ; 二次放电
- 英文论文关键词：The solar array ; Equivalent circuit ; The numerical simulation ; The primary discharge ; The secondary discharge
- 会议召开时间：2015-08-12
- 会议录名称：静电放电：从地面新技术应用到空间卫星安全防护—中国物理学会第二十届全国静电学术会议论文集
- 语种：中文
- 分类号：V442
- 学会代码：WLJD
- 会议名称：静电放电 ; 从地面新技术应用到空间卫星安全防护—中国物理学会第二十届全国静电学术会议
- 会议地点：中国河北石家庄
- 主办单位：中国物理学会静电专业委员会
- 学会名称：中国物理学会静电专业委员会
- 页数：6
- 文件大小：628k
- 原文格式：D
- 会议级别：全国
摘要
空间太阳电池阵静电放电引起的新失效模式会对太阳电池阵带来不良影响。根据等效电路原理建立空间太阳电池阵静电放电模型,通过改变不同元件参数模拟不同情况下空间太阳电池阵静电放电的情况,得到空间太阳电池阵一次放电和二次放电的脉冲电流波形。在空间太阳电池阵一次放电通路中,当电路中电阻值一定时,随着电感的增大,电流脉冲幅值逐渐减小,振荡逐渐增多,脉宽逐渐增大。当电路中电感值一定时,随着电阻的增大,电流脉冲幅值逐渐减小,振荡变化幅度不大,脉宽逐渐减小。在空间太阳电池阵二次放电过程中,电阻值一定时,随着电路中电感的增大,电流脉冲幅值变化不大,振荡逐渐增多,脉宽逐渐增大。研究结果可对空间太阳电池阵安全防护提供一定的理论依据。
Space solar cell array’s new failure caused by electrostatic discharge can bring bad infl uence to the solar cell array.Space solar cell array electrostatic discharge model is set up according to the principle of equivalent circuit,by changing the parameters of different element to simulate space solar cell array’s electrostatic discharge under different conditions,to get the space solar cell array the first discharge and the secondary discharge pulse current waveform.In space solar array’s primary discharge path,when the resistance in the circuit is constant,with the increase of inductance,current pulse amplitude decreases,oscillation increases gradually,pulse width increases gradually.When inductance in the circuit is constant,with the increase of resistance,current pulse amplitude decreases,oscillation amplitude change is not big,pulse width decreases.In space solar array’s secondary discharge path,when the resistance in the circuit is constant,with the increase of inductance in the circuit,the electric current pulse amplitude change is not big,oscillation increases gradually,pulse width increases gradually.The results of the study of space solar array provide certain theoretical basis for safety protection.
Space solar cell array’s new failure caused by electrostatic discharge can bring bad infl uence to the solar cell array.Space solar cell array electrostatic discharge model is set up according to the principle of equivalent circuit,by changing the parameters of different element to simulate space solar cell array’s electrostatic discharge under different conditions,to get the space solar cell array the first discharge and the secondary discharge pulse current waveform.In space solar array’s primary discharge path,when the resistance in the circuit is constant,with the increase of inductance,current pulse amplitude decreases,oscillation increases gradually,pulse width increases gradually.When inductance in the circuit is constant,with the increase of resistance,current pulse amplitude decreases,oscillation amplitude change is not big,pulse width decreases.In space solar array’s secondary discharge path,when the resistance in the circuit is constant,with the increase of inductance in the circuit,the electric current pulse amplitude change is not big,oscillation increases gradually,pulse width increases gradually.The results of the study of space solar array provide certain theoretical basis for safety protection.
引文
[1]刘志全,杨淑利,濮海玲,等.空间太阳电池阵的发展现状及趋势[J].航天器工程,2012,21(6):112-118.LIU Zhiquan,YANG Shuli,PU Hailing,et al.Development and Trend of Space Solar Array Technology[J].Spacecraft Engineering,2012,21(6):112-118
[2]秦文波,程惠尔,李鹏,等.航天器刚性基板太阳电池阵在轨热分析[J].哈尔滨工业大学学报,2008,40(5):827-831.QIN Wenbo,CHENG Huier,LI Peng,et al.Thermal analysis of solar array with rigid substrate on spacecraft in orbit[J].Journal of Harbin Institute of Technology,2008,40(5):827-831.
[3]谢宗武,宫钇成,史士财,等.空间太阳能电池阵列技术综述[J].宇航学报,2014,35(5):491-497.XIE Zongwu,GONG Yicheng,SHI Shicai,et al.A Survey of the Space Solar Array Technique[J].Journal of Astronautics,2014,35(5):491-497.
[4]李鹏,程惠尔.太阳电池阵极月轨道在轨热分析[J].空间科学学报,2006,26(4):303-308.LI Peng,CHENG Huier.Thermal Analysis of the Solar Array in the Lunar Orbit[J].Chinese Journal of Space Science,2006,26(4):303-308.
[5]井琦.太阳电池阵受空间环境的影响及防护[J].电源技术,2008,132(11):787-789.JING Qi.Space environment effects and protects for satellite solar array[J].Chinese Journal of Power Sources,2008,132(11):787-789.
[6]Malone,Patrick K.,Williams,Geoffrey T.Lightweight inflatable solar array[J].Journal of Propulsion and Power,1996,12(5):866-872.
[7]路火平,杨华星,陈诚,等.太阳电池阵EM板热真空试验电路故障测试技术[J].航天器环境工程,2014,31(4):392-396.LU Huoping,YANG Huaxing,CHEN Cheng,et al.Measurement of electrical properties of solar array EMpanel in thermal vacuum test[J]Spacecraft Environment Engineering,2014,31(4):392-396.
[8]METZ.R.N..Circuit transients due to arcs on a high-voltage solar array[J].Journal of Spacecraft and Rockets,1986,23(5):499-504.
[9]童靖宇,刘向鹏,张超,等.CAST2000卫星太阳电池阵基板原子氧防护技术研究[J].装备环境工程,2008,5(6):72-75.TONG Jingyu,LIU Xiangpeng,ZHANG Chao,et al.Study on Atomic Oxygen Protection Coating of Solar Cell Array Panel on CAST2000 Satellite[J].Equipment Environmental Engineering,2008,5(6):72-75.
[10]冯柳,张淑娇,吕伟,等.空间太阳电池组件自动焊接系统[J].电源技术,2014,138(3):478-479.FENG Liu,ZHANG Shujiao,LV Wei,et al.Novel automatic welding machine for space solar module[J].Chinese Journal of Power Sources,2014,138(3):478-479.
[11]Ralph D.Lorenz Solar Array Degradation by Dust Impacts During Cometary Encounters[J].Journal of Spacecraft and Rockets,199835(4):579-582.
[12]黄洪昌,杨运强,李君兰,等.航天器太阳电池阵热-结构分析研究进展[J].电子机械工程,2012,28(4):2-7.HUANG Hongchang,YANG Yunqiang,LI Junlan,et al.Development of Thermal-structural Analysis for Spacecraft Solar Array[J].Electro-Mechanical Engineering,2012,28(4):2-7.
[13]赵颖,刘松喆,金海雯,等.电磁监测卫星太阳电池阵表面等电位控制[J].电源技术,2014,138(2):276-278.ZHAO Ying,LIU Songzhe,JIN Haiwen,et al.Controlling techniques of electrostatic cleanliness in design of solar arrays for electromagnetism survey satellite[J].Chinese Journal of Power Sources,2014,138(2):276-278.
[14]THORNTON.EARL A.,KIM.YOOL A..Thermally induced bending vibrations of a flexible rolled-up solar array[J].Journal of Spacecraft and Rockets,1993,30(4):438-448.
[15]赵长江.航天器太阳电池阵分流技术研究[J].航天器工程,2009,18(3):41-47.ZHAO Changjiang.Technology of Solar Cell Array Shunt-regulation on Spacecraft[J].Spacecraft Engineering,2009,18(3):41-47.
[16]Vladimir E.Skurat,Ilya O.Leipunsky,Ilya O.Volkov.Changes of Solar Array Surfaces on Orbital Station Mir[J].Journal of Spacecraft and Rockets,2011,48(1):53-58.
[17]师立勤,刘四清,郑惠南,等.低轨道航天器高电压太阳电池阵电流泄漏效应分析计算[J].空间科学学报,2012,32(1):130-135.SHI Liqin,LIU Siqing,ZHENG Huinan,et al.Analysis and Calculation for Current Leakage Effect of High Voltage Solar Array in LEO[J].Chinese Journal of Space Science 2012,32(1):130-135.
[18]孙创,夏新林,董士奎,等.外露式星载光电设备在轨热分析[J].宇航学报,2009,30(2):775-779.SUN Chuang,XIA Xinlin,DONG Shikui,et al.Thermal Analysis for Exposed Photoelectric Instrument on Satellite[J].Journal of Astronautics,2009,30(2):775-779.
[19]井元良,王超,雷英俊,等.采用太阳电池阵和储能飞轮的电源系统设计与分析[J].航天器工程,2014,23(3):54-61.JING Yuanliang,WANG Chao,LEI Yingjun,et al.Design and Analysis of Solar Array and Flywheel Power System[J].Spacecraft Engineering,2014,23(3):54-61.
[20]李凯,王立,秦晓刚,等.地球同步轨道高压太阳电池阵充放电效应研究[J].航天器环境工程,2008,25(2):125-128.LI Kai,WANG Li,QIN Xiaogang,et al.Charging and discharging effects on high-voltage solar array in GEO[J].Spacecraft Environment Engineering,2008,25(2):125-128.
[21]李凯,谢二庆,林洪峰,等.空间太阳阵二次放电的模拟实验研究[J].物理学报,2005,54(5):2162-2165.LI Kai,XIE Erqing,LIN Hongfeng.Experimental study on high-voltage and high-powersolar array secondary discharge[J].Acta Physica Sinica,2005,54(5):2162-2165.
[22]杨垂柏,梁金宝,王世金,等.地球同步轨道航天器太阳电池阵静电放电监测方法初探[J].太阳能学报,2008,29(2):135-138.YANG Chuibai,LIANG Jinbao,WANG Shijin,et al.Monitoring method for solar PV array ESD of GEO spacecraft[J].Acta Energiae Solaris Sinica,2008,29(2):135-138.
[23]崔新宇,孙彦铮,王远征,等.高压大功率太阳电池阵防静电措施评价试验[J].电源技术,2004,1(10):644-648.CUI Xinyu,SUN Yanzheng,WANG Yuanzheng,et al.An estimative examination to the hedge electrostatic discharge of high voltage and high power solar array[J].Chinese Journal of Power Sources,2004,1(10):644-648.
[24]Vladimir E.Skurat,llya O.Leipunsky,llya O.Volkov,et al.Changes of Solar Array Surfaces on Orbital Station Mir[J].Journal of Spacecraft and Rockets,2011,48(1):53-58.
[25]PAPULA.P,STOWELL.C..Solar array‘hot-spot’testing and analysis[J].Journal of Spacecraft and Rockets,1986,23(4):401-406.
[26]孙彦铮,刘晓为,唐军,等.太阳电池阵样品等效电容的确定方法[J].电源技术,2005,1(8):542-544.SUN Yanzheng LIU Xiaowei,TANG Jun,et al.Method for determining the equivalent capacitance of solar array sample[J].Chinese Journal of Power Sources,2005,1(8):542-544
[2]秦文波,程惠尔,李鹏,等.航天器刚性基板太阳电池阵在轨热分析[J].哈尔滨工业大学学报,2008,40(5):827-831.QIN Wenbo,CHENG Huier,LI Peng,et al.Thermal analysis of solar array with rigid substrate on spacecraft in orbit[J].Journal of Harbin Institute of Technology,2008,40(5):827-831.
[3]谢宗武,宫钇成,史士财,等.空间太阳能电池阵列技术综述[J].宇航学报,2014,35(5):491-497.XIE Zongwu,GONG Yicheng,SHI Shicai,et al.A Survey of the Space Solar Array Technique[J].Journal of Astronautics,2014,35(5):491-497.
[4]李鹏,程惠尔.太阳电池阵极月轨道在轨热分析[J].空间科学学报,2006,26(4):303-308.LI Peng,CHENG Huier.Thermal Analysis of the Solar Array in the Lunar Orbit[J].Chinese Journal of Space Science,2006,26(4):303-308.
[5]井琦.太阳电池阵受空间环境的影响及防护[J].电源技术,2008,132(11):787-789.JING Qi.Space environment effects and protects for satellite solar array[J].Chinese Journal of Power Sources,2008,132(11):787-789.
[6]Malone,Patrick K.,Williams,Geoffrey T.Lightweight inflatable solar array[J].Journal of Propulsion and Power,1996,12(5):866-872.
[7]路火平,杨华星,陈诚,等.太阳电池阵EM板热真空试验电路故障测试技术[J].航天器环境工程,2014,31(4):392-396.LU Huoping,YANG Huaxing,CHEN Cheng,et al.Measurement of electrical properties of solar array EMpanel in thermal vacuum test[J]Spacecraft Environment Engineering,2014,31(4):392-396.
[8]METZ.R.N..Circuit transients due to arcs on a high-voltage solar array[J].Journal of Spacecraft and Rockets,1986,23(5):499-504.
[9]童靖宇,刘向鹏,张超,等.CAST2000卫星太阳电池阵基板原子氧防护技术研究[J].装备环境工程,2008,5(6):72-75.TONG Jingyu,LIU Xiangpeng,ZHANG Chao,et al.Study on Atomic Oxygen Protection Coating of Solar Cell Array Panel on CAST2000 Satellite[J].Equipment Environmental Engineering,2008,5(6):72-75.
[10]冯柳,张淑娇,吕伟,等.空间太阳电池组件自动焊接系统[J].电源技术,2014,138(3):478-479.FENG Liu,ZHANG Shujiao,LV Wei,et al.Novel automatic welding machine for space solar module[J].Chinese Journal of Power Sources,2014,138(3):478-479.
[11]Ralph D.Lorenz Solar Array Degradation by Dust Impacts During Cometary Encounters[J].Journal of Spacecraft and Rockets,199835(4):579-582.
[12]黄洪昌,杨运强,李君兰,等.航天器太阳电池阵热-结构分析研究进展[J].电子机械工程,2012,28(4):2-7.HUANG Hongchang,YANG Yunqiang,LI Junlan,et al.Development of Thermal-structural Analysis for Spacecraft Solar Array[J].Electro-Mechanical Engineering,2012,28(4):2-7.
[13]赵颖,刘松喆,金海雯,等.电磁监测卫星太阳电池阵表面等电位控制[J].电源技术,2014,138(2):276-278.ZHAO Ying,LIU Songzhe,JIN Haiwen,et al.Controlling techniques of electrostatic cleanliness in design of solar arrays for electromagnetism survey satellite[J].Chinese Journal of Power Sources,2014,138(2):276-278.
[14]THORNTON.EARL A.,KIM.YOOL A..Thermally induced bending vibrations of a flexible rolled-up solar array[J].Journal of Spacecraft and Rockets,1993,30(4):438-448.
[15]赵长江.航天器太阳电池阵分流技术研究[J].航天器工程,2009,18(3):41-47.ZHAO Changjiang.Technology of Solar Cell Array Shunt-regulation on Spacecraft[J].Spacecraft Engineering,2009,18(3):41-47.
[16]Vladimir E.Skurat,Ilya O.Leipunsky,Ilya O.Volkov.Changes of Solar Array Surfaces on Orbital Station Mir[J].Journal of Spacecraft and Rockets,2011,48(1):53-58.
[17]师立勤,刘四清,郑惠南,等.低轨道航天器高电压太阳电池阵电流泄漏效应分析计算[J].空间科学学报,2012,32(1):130-135.SHI Liqin,LIU Siqing,ZHENG Huinan,et al.Analysis and Calculation for Current Leakage Effect of High Voltage Solar Array in LEO[J].Chinese Journal of Space Science 2012,32(1):130-135.
[18]孙创,夏新林,董士奎,等.外露式星载光电设备在轨热分析[J].宇航学报,2009,30(2):775-779.SUN Chuang,XIA Xinlin,DONG Shikui,et al.Thermal Analysis for Exposed Photoelectric Instrument on Satellite[J].Journal of Astronautics,2009,30(2):775-779.
[19]井元良,王超,雷英俊,等.采用太阳电池阵和储能飞轮的电源系统设计与分析[J].航天器工程,2014,23(3):54-61.JING Yuanliang,WANG Chao,LEI Yingjun,et al.Design and Analysis of Solar Array and Flywheel Power System[J].Spacecraft Engineering,2014,23(3):54-61.
[20]李凯,王立,秦晓刚,等.地球同步轨道高压太阳电池阵充放电效应研究[J].航天器环境工程,2008,25(2):125-128.LI Kai,WANG Li,QIN Xiaogang,et al.Charging and discharging effects on high-voltage solar array in GEO[J].Spacecraft Environment Engineering,2008,25(2):125-128.
[21]李凯,谢二庆,林洪峰,等.空间太阳阵二次放电的模拟实验研究[J].物理学报,2005,54(5):2162-2165.LI Kai,XIE Erqing,LIN Hongfeng.Experimental study on high-voltage and high-powersolar array secondary discharge[J].Acta Physica Sinica,2005,54(5):2162-2165.
[22]杨垂柏,梁金宝,王世金,等.地球同步轨道航天器太阳电池阵静电放电监测方法初探[J].太阳能学报,2008,29(2):135-138.YANG Chuibai,LIANG Jinbao,WANG Shijin,et al.Monitoring method for solar PV array ESD of GEO spacecraft[J].Acta Energiae Solaris Sinica,2008,29(2):135-138.
[23]崔新宇,孙彦铮,王远征,等.高压大功率太阳电池阵防静电措施评价试验[J].电源技术,2004,1(10):644-648.CUI Xinyu,SUN Yanzheng,WANG Yuanzheng,et al.An estimative examination to the hedge electrostatic discharge of high voltage and high power solar array[J].Chinese Journal of Power Sources,2004,1(10):644-648.
[24]Vladimir E.Skurat,llya O.Leipunsky,llya O.Volkov,et al.Changes of Solar Array Surfaces on Orbital Station Mir[J].Journal of Spacecraft and Rockets,2011,48(1):53-58.
[25]PAPULA.P,STOWELL.C..Solar array‘hot-spot’testing and analysis[J].Journal of Spacecraft and Rockets,1986,23(4):401-406.
[26]孙彦铮,刘晓为,唐军,等.太阳电池阵样品等效电容的确定方法[J].电源技术,2005,1(8):542-544.SUN Yanzheng LIU Xiaowei,TANG Jun,et al.Method for determining the equivalent capacitance of solar array sample[J].Chinese Journal of Power Sources,2005,1(8):542-544