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3、:参考http:/WWW(b) -80 -90-100 N -IlO W -120 2 -130-1400引言（从。开始顺序编号）文章整体逻辑结构依次为：引言，原理（算法），实验（装置/模拟），结果（分析与讨论），结论（展望）。请保证每个英文简写（包括图表当中）在第一次出现时都有其对应的中文（或英文）全称。引言内容包含：（1）必要的研究背景介绍；（2）国内外已有研究成果描述；（3）基于己有成果进一步研究动机；（4）作者研究的目的；（5）简述作者的主要研究工作；（6）研究结果的意义。引言中不建议出现图、表以及公式；慎用“首次”、“第一次”等词语；引言不能过长，超过一页要考虑精简;切忌与摘要和结论
4、重复;文中出现的单位名称请使用全称，最常见的如“中科院”应写为“中国科学院”。论文中参考文献标注序号根据文献在正文中一次被引用的先后次序来编号。多次引用的同一文献用同一编号。编号除非属正文描述，否则都用上标表示，如：“某某明，”。1原理实验分析1.1 二级序号1.1.1 三级序号正文中应出现对所有图片的描述文字（不用交叉引用功能），并在正文相应位置放置图片，图片应放置在正文引用后面，避免背题，图片需按出现顺序编号。正文中可使用诸如：“如图1（a）所示”、“见图1”等。实例如图1所示。FrcqucncyZMHz图1 （a）基于半导体光放大器与自注入锁定技术的单 频光纤激光器全光噪声抑制实验装置图
5、；（b）单频激光 在自由运转以及半导体光放大器和自注入锁定技术应收稿日期：2022-XX-XX：修订日期：2022-XX-XX基金项目：国家自然科学基金（62105240,62075159）：国家重点研发计划（2019YFB2203002）作者简介：姓名，性别，职称,学历，生要从事KX方面的研究。邮箱导师简介：姓名，性别，职称，学历，主要从事XX方面的研究。（第一作者为学生的须填写导师信息）通讯作者：姓名，性别，职称，学历，主要从事XX方面的研究。邮箱（当导师通讯作者为同一人时，请写：“导师（通讯作者简介”。用下噪声特性对比图川Fig.7(a)Experimentalsetupofthelow
6、-noisesingle-frequencyfiberlaserbasedonboosteropticalamplifier(BOA)andself-injectionlocking(SIL)techniques;(b)Comparisononlasernoiseofthesingle-frequencylaserunderfree-runningstatus,andnoisecontrolstatuswithBOAandSILtechniques111图片要求分辨率达600dpi,曲线图或流程图等，要求图中字符、刻度清晰可见；图片的宽度通栏在1114cm,双栏在67.5cm;图片中文字须全部
7、改为英文，所有英文词组首字母大写；图题要求中英文对照，中前英后，图题的描述内容要求与正文一致；有分图时，分图请用(a)(b)(c)标出，坐标图刻度标值线在内侧，刻度清晰，标值明确。坐标标目应由物理量和单位组成，标记形式如WaVeIengIhnmo物理量名称和符号应与正文一致，并在正文中有说明。XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
8、XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
9、XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
10、XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
11、XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXO双栏图片中文字若太小无法辨认,请改为通栏显示，保证插图内文字清晰，如图2所示。793nmPUmPPMTDFK)/130何CMSo)o)o505052211MuV6M0d三d30OSSWdOl-1-1-110.80
12、.91.01.11.2131.41.5PumppoweratI570nm/W300(b)350IUgP-HW三图2(a)基于掺铁.布里渊复合增益的2m窄线宽单频光纤激光器实验装置图：(b)单频激光功率输出曲线，插图:基于延迟自外差法测得的斯托克斯光线宽Fig.2(a)Experimentalsetupofthe2mnarrow-linewidthsingle-frequencyBrillouin-Thulium-basedfiberlaser;(b)Curvesofsingle-frequencylaseroutputpower;Inset:MeasuredStokeslinewidthbas
13、edondelayedself-heterodynemethod111文中易混淆的大小写，上、下角标，文种、算符的字母,请注明清晰;物理量单位用正体，物理量符号用斜体；对于向量和矩阵变量，需要使用粗斜体；物理量符号需全文一致(包括图，表及公式)。物理量的含义需在第一次出现时予以说明。一个物理量只用唯一字母符号表示，多个字母符号不能代表同一变量。公式在文章中以阿拉伯数字连续编号，用()括起置于公式右边；公式中的所有物理量均需给出物理意义；先出现公式，再在正文中给出关于公式的描述。Tl=cos(1)式中：TI为XXX；cos6为XXX；Aa为XXX。其中，符号*仅用于表示卷积，公式中乘号可选择点乘
14、或叉乘X。正文中应出现对所有表格的描述文字，并在正文相应位置放置表格，表格需按出现顺序编号；表中的文字请使用英文表示，题目需要中英文对照；物理量需提供名称、与物理量相应的符号以及单位。如：WavelcngthZnmo表1表采用三线表的格式(必要时可加辅线)Tab.1英文与中文保持一致ThicknessZnmTime/sRelativeerror0.5-293.8+0.60.18%1.1-3.4347.80.60.45%2结论不同于摘要部分的结论内容，应该详细、清楚，能使读者通过这一部分了解作者工作的意义所在，与其他人的工作的比较，存在的问题以及对未来前景的展望。注意：不能出现图、表及公式，尽量
15、不出现文献引用。XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX参考文献：文献数量1520条为宜,需引用正式发表的文献，以确保读者能找到所引文献。中文文献如存在对应英文信息，需给出，按照英文在前，中文在后的顺序列出，并在英文信息最后添加“(inChinese)”。若文献本身没有英文对应信息，请勿自行翻译，给出中文即可。所引
16、文献作者需列出前三位，超过三位作者的在第三位作者后加“等”，英文为“etal”；刊名缩写请使用常用缩写形式,缩写后不加中文期刊的英文名称不得使用缩写；每条文献末用结束；作者姓名均采用姓前名后的形式，英文文献中作者可用“姓的全称名的首字母”表示(名缩写后无)，中文文献作者姓名需写全称。多个作者之间用逗号分开，最后一个作者之前无“and”；单篇页码形式的期刊，页码为一个数字，页码写出该数字即可；非书籍英文文献题目，除第一个单词首字母、人名、术语、缩写等外，其余单词首字母均小写，对于书籍类文献，题目中所有单词首字母均大写；请作者保留引用文献的电子版，编辑部可能会索要，以便核对信息。以下实例可作为参考
17、：期刊1 ShiWei,FuShijie,ShengQuan,etal.Researchprogressonhigh-perfonnancesingle-frequencyfiberlasers:2017-2021(Invited)J.InfraredandLaserEngineering.2022,51(1):20210905.(inChinese)doi:103788IRLA20210905史伟，付士杰，盛泉，等.高性能单频光纤激光器研究进展：2017-2021(特邀)J.红外与激光工程，2022,51(1):20210905.doi:10.3788/IRLA20210905会议2 McM
18、anusHughL.Controlofspacestructurethermaldeformation:AnoverviewCProcofSPIE,1993,1917:545-554.报告3 TesslerA,SpanglerJL,MattoneM,etal.Real-timecharacterizationofaerospacestructuresusingonboardstrainmeasurementtechnologiesandinversefiniteelementmethod(R.NASA,0704-0188.2011.学位论文4 ChenS.Researchondeformati
19、onmeasurementandreconstructionmethodforcompositestructuresbasedonsirainsD.Xi,an:XidianUniversity,2018.(inChinese)图书5 ZhuXS,Chavez-PirsonA,MilaneseD,etal.Non-SilicaOxideGlassFiberLaserSources:PartIIIM!/AdvancesinGlassScienceandTechnology.NewYork:IntechOpen,2018.电子文献6 GareP,NelmsN.NowickiY.Requirement
20、s,developmentsandchallengesforCCDandCMOSimagesensorsforspaceapplicationsEBOL.(2013-12-16)2015-05-25http:/www.imagesensors.org.专利7 刘加林.多功能一次性压舌板：中国，92214985.2P.1993-04-14.标准8 全国文献工作标准化技术委员会第七分委员会.GB/T57951986中国标准书号S).北京：中国标准出版社，1986.科研论文英文长摘要模板DesignofportableinfraredtargetsimulatorsystemGaoHongwei,Y
21、angZhongming2,LiuHongbo3,ZhuangXingang3,LiuZhaojun21 KeyLaboratoryofLaserandInfraredSystem,ShandongUniversity,Qingdao266237,China;2 SchoolofInformationScienceandEngineering,ShandongUniversity,Qingdao266237,China;3 The41stInstituteofChinaElectronicsTechnologyGroupCorporation,Qingdao266555,ChinaAbstra
22、ctObjectiveInfraredtargetsimulatorisanimportantpartofinfraredtargetsimulationexperiment.WhentheoutgoingpupiloftheColIimalionsystemcoincideswiththeincidentpupilofthedetectionequipment,itcanprovideastableinfinitelyfarsimulatedtargetforinfrareddetectionequipment,andthesimulationresultshavetheadvantages
23、ofbeingaccurate,controllableandrepeatableexperiments,whichareusedtoevaluatetheperformanceandaccuracyofinfrareddetectionequipment.Thereareimportantapplicationsinradarlest,infraredguidance,infraredtracking,etc.Withthedevelopmentofphotoelectricdetectionequipmentsensorintegrationandminiaturization,multi
24、-bandsensorshavebecomethestandardconfigurationofmostphotoelectricdetectionequipment.Duetochangesinthedebuggingenvironmentandtheuseoftheenvironment,itisnecessarytoadjustitfrequently,butmostofthetargetsimulatorsinthelaboratoryareonlyequippedwithasingle-bandlightsource,largesizeisnotconvenienttocarry.T
25、herefore,itisnecessarytoestablishmulti-bandandsmall-sizedportabletargetsimulatorstomeettheneedsofdifferentusageenvironments.Forthispurpose,anoff-axisreflectiveinfraredtargetsimulatorsystemisdesignedinthispaper.MethodsAportableinfraredtargetsimulationsystemisbuiltinthispaper.A110mmapertureparallellig
26、httubeofreflectivestructureischosenasthecollimationsystem(Fig.2).Theoptical-mechanicalthermalintegrationanalysisofthesystemisperformedtodetermine(hedeformationvariationoftheprimaryandsecondarymirrorsandmechanicalstructurecausedbytemperaturedifference(Fig.8).Theself-collimatinginterferometricdetectio
27、nmethodismountedusingaZygointerferometer(Fig.11),andthemountingresultsarejudgedbythePVandRMSvalueresultsofthefaceshapemeasurementofthestandardplanemirror(Fig.13).ResultsandDiscussionsTheportableinfraredtargetsimulationsystemismountedusingself-collimatinginterferometry,withPVvalueof0.3562andRMSvalueo
28、f0.047z(Fig.13),whichisbetterthan20,andtheresultsareexcellentandmeettheusagerequirements.TheresultsofZemikecoefficientanalysisshowthatthesystemaberrationsaremainlyout-of-focus,tiltandhigherorderaberrationsofmorethan5levels(Tab.5),andtheadjustabletargetdiscisdesignedtocompensateandimprovetheimagingqu
29、ality.Aportableinfraredtargetsimulationsystemisbuiltinthelaboratorytotesttheopticalpathandverifytheimagingfunctionofthesystem.Theinfraredcameraandheadareplacedatadistanceof10mfromthesystem,andtheimagingresultsareshown(Fig.14).Thetargetsofdifferentshapescanbeclearlyidentified,andtheimagingfunctionoft
30、hesystemsatisfiesthedemandofsimulatingtargetsatinfinity.ConclusionsAportableinfraredtargetsimulationsystemwithworkingwavelengthsof3-5mand8-14misdesigned.Thesystemischaracterizedbysimplestructure,adjustablewavelength,richtarget,clearandstableimaging.ThewavefrontqualityofthesystemisanalyzedusingZemaxs
31、oftware,andthePVvalueofthecentralfieldofviewis0.0132%andtheRMSvaluewas0.0038zinthe4-mband,andthePVvalueofthecentralfieldofviewis0.0044zandtheRMSvalueis0.00132inthe12-mband.Anoptical-mechanicalthermalanalysisofthecollimationsystemisperformed,andatatemperaturedifferenceof30,thedeformationcausedbytheme
32、chanicalstructureismuchlargerthanthedeformationoftheprimaryandsecondarymirrorsthemselves,reachingtheorderof10m,andtheimagingresultshaveobviousout-of-focuserrors,whichcanbecompensatedfortheout-of-fbeuserrorsintroducedbythetemperaturechangebyrefocusingthetargetdiscwithadjustablethree-dimensionalpositi
33、on.Theimagingfunctionofthesystemistested.Fordifferentshapesoftargets,thesystemcanbecomeaclearandidentifiableimage,providingastablesimulatedtargetforinfrareddetectionequipment.Keywords:opticalengineering;targetsimulator;opticaldesign;collimatorFundingprojects:NaturalScienceFoundationofChina(No.*)综述英文
34、长摘要模板Asurveyonlaserintersatellitelink:Currentstatus,trends,andprospects1.iRUilNLinBaojunh2345,LiuYingchun1-25,ShenYuan25,DongMing-ji25,ZhaoShuai25,KongChenjie25,LiuEnquan2,5,LinXia2,5(1.UniversityofChineseAcademyofSciences,Beijing100049,China;2. InnovationAcademyforMicrosatellites,ChineseAcademyofSc
35、iences,Shanghai200135,China;3. ShanghaiTechUniversity,Shanghai201203,China4. AerospaceInformationResearchInstitute,ChineseAcademyofSciences,Beijing100094,China5.ShanghaiEngineeringCenterforMicrosatellites,Shanghai201210,China)Abstract:SignificanceThehighdirectionalityandshortwavelengthoflasertransmi
36、ssioninspacemakeitapromisingdirectionforthenextgenerationofsatellitelasercommunication.Thelaserintersatellitecommunicationcanachievehighquality-of-servicesatellitecommunicationwithhightransmissionspeed,widebandwidth,andhighsecurity,whichcanevenimprovetheprecisionofsatelliteranginginspace.Theestablis
37、hmentofasatellitebackbonenetworkwithlaserintersatellitelinkscanachieveglobalmanagementandcontrolofsatellites,greatlyimproveitsindependencefromthegroundsystem,andexpandthecommunicationcapacity.Duetoitsadvantagesinimprovingthesurvivability,autonomy,mobilityandflexibilityofsatellitenetworks,thedomestic
38、StarNetwork,Hongyanu,Hongyunr,XingyunandSpace-EarthIntegrationconstellationsandforeignKuiper,TelesatandStarlinknetworkshaveintegratedlaserinter-satellitelinksasoneofitscoretransmissionlinkmethods,lasercommunicationterminalsalsobecomeoneofthestandardspacecraftpayloads.Itisforeseeablethatinter-satelli
39、tecommunicationwillcontinuetodevelopandtransformfromtheradiowaveeratothelaserera,whichmakesthesurveyonlaserintersatellitelinksmeaningful.ProgressFirst,thetechnicalfundamentsisintroduced,includingthelinkestablishmentmodes,linkmodulationmodes,andwavelengths.Theinter-satellitelaserlinkestablishmentmain
40、lyreliesonthethreestepsofpointing,acquiring,andtracking,comprehensivelycalledPATsystem.Thelinkmodulationmodesincludenon-coherentandcoherentcommunications.Comparedwiththenon-coherentsystem,thecoherentsystemhastheadvantagesofhighspectralefficiency.Formediumandhigh-orbitsatellitesthatneedtocarrymorecom
41、plexandsophisticatedcommunicationtasks,thelaserinter-satellitelinkismostlymodulatedbythecoherentcommunicationsystem.Conversely,low-orbitsatellitelasercommunicationanddeepspaceexplorationprojectsmainlyusenon-coherentmodulationmode.Tbreducetheimpactofthesolarbackgroundandsolarscattering,thecurrentlase
42、rcommunicationmainlyconsiderstheselectionintherangeof500nmto2000nm.Sincegroundindustrial-gradelasercomponentsmostlyuse1550nmwavelengthlaserasastandardpreparation,thecommunicationtechnologycanbemigratedtothesatellitenetworkatarelativelylowcost.Withthedevelopmentoftechnology,thecommunicationsystemsofv
43、ariouscountriesaredevelopinginamorecompatibledirection,thatis,compatiblewithboth1064nmand1550nmwavelengths.Countrieshavesuccessfullycarriedoutanumberofon-orbittechnologyverificationsinthefieldofinter-satellitelasercommunication,andhaveenteredthestageoflarge-scaleapplication.Thesurveyfindsthatthecurr
44、enton-orbittechnologyverificationusescustomizedlaserterminalstomeetthespecificneedsofvarioustasks.CompaniessuchasMynaric,HyperionTech,ThalesAleniaSpace,andNICThavebeguntolaunchlaserterminalproductswithhigherspeed,smallermassandvolume,andlowerpowerconsumption.Theseterminalproductscanadapttotheunivers
45、alrequirementsofsimilarmulti-tasking.Accordingtothedifferentmissionrequirementsofdifferentorbitheights,thecurrentdevelopmentstatusandplansoflasercommunicationachievementssince2015issummarized(Tab.1).Throughthecomprehensivesurvey,thispaperrevealstheflexibilityandmodularitytrendsoflasercommunicationte
46、rminals,andfourdevelopmenttrendsofsatellitelasercommunication:standardization,compatibility,networking,andcommercialization.Inadditiontobeingusedasacarrierforinformationinteraction,laserrangingcanobtainmoreaccurateinter-satelliterangingvalues,strongeranti-interferenceandanti-eavesdroppingcapabilitie
47、scomparedtotraditionalRFrangingsolutions.Theendofthispapersurveysonprospectsofsatellitelaserrangingapplications,whichintendstoprovidereferencetothedomesticdevelopmentandresearchoflaser-basedsatellitetechnology.ConclusionsandProspectsThelaserinter-satellitelinkisdevelopingvigorously.Atthesametime,the
48、missionrequirementsofthesatellitenetworkarecomplexanddiverse.Forsatellitesofdifferentorbitsandmissiontypes,theselectionofthecommunicationsystem,wavelength,andaccessmodeofthelaserinter-satellitelinkneedstobeanalyzedindetailaccordingtoeachsituation.Theresearchofthispaperaimstoprovidesomereferenceandreferenceforthedesignandoptimizationoflaserinter-satellitelinksinthefuture.Itisexpectedthatbuildingastandardized,compatible,networkedandcommercializedlaseri
