简介:Acertainnumberofconsiderationsshouldbetakenintoaccountinthedynamiccontrolofrobotmanipulatorsashighlycomplexnon-linearsystems.Inthisarticle,weprovideadetailedpresentationofthemechanicalandelectricalimpli-cationsofrobotsequippedwithDCmotoractuators.Thismodeltakesintoaccountallnon-linearaspectsofthesystem.Then,wedevelopcomputationalalgorithmsforoptimalcontrolbasedondynamicprogramming.Therobot’strajectorymustbepredefined,butperformancecriteriaandconstraintsapplyingtothesystemarenotlimitedandwemayadaptthemfreelytotherobotandthetaskbeingstudied.Asanexample,amanipulatorarmwith3degreesoffreedomisanalyzed.
简介:Adistributedcontrolsystemisdesignedforplasmasprayingequipmentandtheconfigurationsofsystemsoftwareandhardwareisdiscussed.Throughfoundinganexpertdatabase,thesprayingprocessparametersareworkedoutandtheinitializationandcontrolofsprayingprocessarerealized.Theplasmasprayingsystemwiththiscontrolconfigurationcansimplifythesprayingoperation,improveautomationlevelofsprayprocess,andapproachtheexperiencecriterionassoonaspossible.
简介:ChemicalfluxesofAsianriversintooceansbeardifferentregionalvariations.Threezonesarecharacteristicofdistinctdissolvedsedimentloadsandyieldsandionicconcentration.RiversintooceansinChinaplayanimportantroleinAsiabecauseoftheirdifferentchemicalfluxes,amongwhichthosedrainingtheLoessPlateauhavehighionicconcentration,lowwaterdischargesanddissolvedsedimentloadsandyields.Climate,vegetation,soilandstratalithology,chemicalweatheringintensityandtectonicactivitydominatechemicalfluxesofAsianriversintooceans,anddifferentfactorshavedifferenteffectsonthechemicalfluxesofseparateregionalrivers.RisingoftheTibetPlateaualsoexertsanimportantinfluenceonchemicalcompositionsofriversoriginatingfromit.
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.
简介:MajorFactorsControllingCalciteDissolutioninHydrothermalKarstSystemsWangYanxin;TangZhonghua(FacultyofEnvironmentalScienceandGe...
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简介:Thesynthesisofultrafineceriumdioxideprecursorviahomogeneousprecipitationwasstudied.Mixedaqueoussolutionofanhydrousceriumnitrateandureawasfirstheatedto85℃for2h,andthepreparedsuspensionwasthenagedatroomtemperatureforvariousperiodsoftime.Whiteprecipitatewasfinallycollectedbycentrifugingandwashedwithdistilledwaterandanhydrousethanol.Theobtainedceriumdioxide(CeO2)precursorwasobservedwithSEM.Itwasfoundthatthemorphologyandsizeoftheprecursorwerestronglyaffectedbyagingtimeandstirringconditions(withorwithoutstirring).Theprecipitatedfinesphericalparticlesoftheprecursorchangedtheirshapefromellipsetosliceordirectlytoslice.Finesphericalmonodispersed(300nm)precursorpowderscouldbeobtainedbycontrollingtheagingtime.Stirringthesolutionalsocouldchangethereactionprocessandthusthemorphologyandsizeoftheprecursorwerechanged.
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