简介:BasedonEvans’spatialsmoothingpreprocessingscheme,anewapproachcalledtwo-directionspatialsmoothingpreprocessingmethodispresented.Itisprovedthatthedecorre-lation,theeffectiveapertureandthemaximumnumberofdistinguishablecoherentsignals(whenarraysizeisgiven)ofthenewmethodarebetterthanthoseoftheEvans’method.Simulationresultsgiveacomparisonbetweentheeigenvectorspectrumsproducedbythetwomethods.
简介:在这份报纸,我们为algebroid功能w(z)证明那,单个方向argz=0,令人满意那为任意并且任何给定的抓住与至多可能的2v非凡的价值一,是w(z)的Nevanlinna方向。
简介:Themainpurposeofthispaperistoprovidearestartingdirectionforimprovingonthestandardconjugategradientmethod.Ifadrasticnon-quadraticbehaviouroftheobjectivefunctionisobservedintheneighbourofxk,thenarestartshouldbedone.Thescalingsymmetricrank-oneupdatewithDavidon’soptimalcriterionisappliedtogeneratetherestartingdirection.Itisprovedthattheconjugategradientmethodwiththisstrategyretainsthequadratictermination.Numericalexperimentsshowthatitissuccessful.
简介:Inthispaper,alowcomplexityESPRITalgorithmbasedonpowermethodandOrthogo-nal-triangular(QR)decompositionispresentedfordirectionfinding,whichdoesnotrequireaprioriknowledgeofsourcenumberandthepredeterminedthreshold(separatesthesignalandnoiseei-gen-values).Firstly,accordingtotheestimationofnoisesubspaceobtainedbythepowermethod,anovelsourcenumberdetectionmethodwithouteigen-decompositionisproposedbasedonQRde-composition.Furthermore,theeigenvectorsofsignalsubspacecanbedeterminedaccordingtoQmatrixandthenthedirectionsofsignalscouldbecomputedbytheESPRITalgorithm.Todeterminethesourcenumberandsubspace,thecomputationcomplexityoftheproposedalgorithmisapproximatedas(2log_2n+2.67)M~3,wherenisthepowerofcovariancematrixandMisthenumberofarrayele-ments.ComparedwiththeSingleVectorDecomposition(SVD)basedalgorithm,ithasasubstantialcomputationalsavingwiththeapproximationperformance.Thesimulationresultsdemonstrateitseffectivenessandrobustness.
简介:Inthispaper,thesubspacefittingmodelsfordirection-of-arrival(DOA)estimationisanalyzed,aneffectivealgorithmicapproachisgiven.Astheinitializationvalueissocriticaltotheglobalconvergence,thecontinuationtheoryisalsousedtodevelopanewframeworkwhichsolvestheinitializationproblempowerfully.Somenumericalevidencewillbegiventoshowthattheperformanceofthenewalgorithmisverypromising.
简介:Sincetheexcessivecapacityinsteelmakingandcontinuouscastingatpresent,andthelimiteddevelopmentmarginofCCtechnologyandequipmentinscale,thefurtherdevelopmentmustbemadeinaprofoundanddetailizedway.ThispaperenumeratestheitemsofCCtechnologyandequipment,whichneedtobedetailizedfromseveralaspectssuchasrollarrangementdesign,equipmentdesignandproductionoperation,anditpointsoutthatdetailizationisthefuturedirectionofCCtechnologyandequipment.Theitemsinrollarrangementdesignincludeeliminatingperiodicmeniscusfluctuationbyadjustingspacebetweenrollsreasonably;takingspecialmeasurestoavoiddangerousregionsofcastingspeed,inordertoreducethecenterporosityandcenterlinecrackofslab;optimizingthemajorradiusandthelengthofouterarcofcasterbeforestraighteningpointtoavoiddangerousregionofcastingspeed.Theitemsinequipmentdesignincludechoosingasuitablestructureofsupportandguidingrollaccordingtotheconcreteconditionsofcaster;accordingtobulgingshapeofslab,thinkingmoreaboutrestrictionofshelltobulgingforce,discussingtheforceonrollers,optimizingsplitrolltosupportslab;safetyfactorshouldbeconsideredtogetherwithcalculationmethodofthebearingnominalstaticload.Theitemsinaspectsofcontinuouscastingoperationincludethedelicacydivisionandthefunction-positioningofoperationmodesforCCmachineduetotheconsiderationofdynamicsoftreduction;monitoringandcontrollingsystemofCCmachinemustbefurtherdetailizedtoimprovethestabilityofproductionoperationandslabquality.Inadditiontothethreeaspectsmentionedabove,thisarticlepointsoutmanyotheritemsalso,suchashomogenizationofsecondarycoolingofslab,qualitycontrolofsurfaceandinternalofslab,andsoon.Thisarticleemphasizes,somekeytechnologiesneedtoberesearchedalso,andalltheseresearcheswillneverstop.
简介:Directionisacommonspatialconceptthatisusedinourdailylife.Itisfrequentlyusedasaselectionconditioninspatialqueries.Asaresult,itisimportantforspatialdatabasestoprovideamechanismformodelingandprocessingdirectionqueriesandreasoning.Dependingonthedirectionrelationmatrix,aninverteddirectionrelationmatrixandtheconceptofdirectionpre-dominanceareproposedtoimprovethedetectionofdirectionrelationbetweenobjects.Directionpredicatesofspatialsystemsarealsoextended.Thesetechniquescanimprovetheveracityofdirectionqueriesandreasoning.Experimentsshowexcellentefficiencyandperformanceinviewofdirectionqueries.
简介:Apracticalmethodforcomputingtheone-wayrectangularorthotropicplate(isotropicplateasaspecialcase)issuggestedinthispaper.Thesupportedcondi-tionsintwooppositeedgesmaybesimplysupported,continuousorsupportednonsymmetricallyandtheothertwooppositeedgesareslide-supportedorfree.Aseriesofsimplifiedformulasaregivenforcalculatingthebendingmomentsalongthecrosssection(loadedsection),inwhichtheactingpointoftheconcentratedloadorthecenterofarec-tangularuniformloadislocated.Thevalidrangeandaccuracyoftheseformulaswerestud-iedandtheapproximateresultswereexaminedandcomparedextensivelywiththosebythetriangularseriessolutionorfiniteelementmethod.
简介:Theproblemconsideredinthispaperistointerpolateavirtualuniformarrayfromarealtwo-dimensionalarraywitharbitrarygeometryviaaninterpolationmatrix.Thekeytothisproblemishowtoarrangethesevirtualsensors.Itisshownthatthevirtualuniformlineararrayshouldhavethesamemain-lobebeam-patternastherealarrayoveranangularsectorofinterest.Simulationresultsarepresentedtoillustratetheapplicationofvirtualarrayindirectionfinding.
简介:Theattitudecontrolsystemdesignanditscontroleffectareaffectedconsiderablybythemass-propertyparametersofthespacecraft.Inthemissionofon-orbitservicing,asfuelisexpended,orthepayloadsareaddedorremoved,thecenterofmasswillbechangedincertainaxe;consequently,somethrusters’directionsaredeviatedfromthecenterofmass(CM)incertainplane.TheCMofassembledspacecraftestimationandthrusterdirectioncontrolarestudied.Firstly,theattitudedynamicsoftheassembledspacecraftisestablishedbasedontheNewton-Eulermethod.Secondly,theestimationcanbeidentifiedbytheleastrecursivesquaresalgorithm.Then,aschemetocontrolthethrusters’directionsisproposed.Byusingthegimbalinstalledattheendoftheboom,theangleofthethrusteriscontrolledbydrivingthegimbal;therefore,thrusterscanbedirectedtotheCMagain.Finally,numericalsimulationsareusedtoverifythisscheme.Resultsofthenumericalsimulationsclearlyshowthatthiscontrolschemeisrationalandfeasible.