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中国空间科学技术
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25 April 2012, Volume 32 Issue 2
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Method of Autonomous Celestial Navigation Based on UKF and Information Fusion
LUO Nan, XU Lu-Ping, ZHANG Hua
2012, 32 (
2
): 1-9. doi:
10.3780/j.issn.1000-758X.2012.02.001
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2282
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X -ray pulsars navigation uses the time of arrival (TOA) of the X-ray pulse radiation to resolve the position. Star sensor based navigation uses the angle between line of sight to the star and the center of earth to resolve the position. The mechanisms of the two navigation systems are different from each other. An information fusion celestial utonomous navigation method was proposed by hybriding the pulsars TOA and elevation angle of star sensor measurement. And the simulation experiments based on unscented Kalman filter (UKF) using real orbit parameters were carried out. A hard-in-loop simulation system which uses the laser quantum to emulate the X-ray quantum of pulsars was designed to test the method. The results show that, comparing to the methods based on pulsars or star sensor only, the estimation accuracy of position and velocity of the proposed method can increase 52.7%, 43.6%, 82.2% and 70.5% respectively, and its performance is better than extended Kalman filter (EKF) information fusion method.
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BudgetAnalysisandSimulationofInter-satelliteLinkinWalker-δConstellation
HAN Song-Hui, GUI Qing-Ming, LI Jian-Wen, DU Yuan-Lu
2012, 32 (
2
): 10-16. doi:
10.3780/j.issn.1000-758X.2012.02.002
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2758
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There is a need for more discussion on the other transmission loss and a reasonable transmission power of inter-satellite link (ISL). Firstly, the criteriafor ISL establishment were given under the agreement of short average distance and small range of ISL azimuth, elevation angleanddistance.Secondly, the budget of the ISL, the free spacepropagationlossandothertransmissionlosswerediscussed,andthereferencevalueor the formulaofthesetransmissionlosseswasgivenlater.Furthermore,areasonabletransmissionpowerwas given bythe probabilisticknowledgeundertheconditionthatthemathematicalexpectationofthepracticaldatawasequaltotherateddataofthetransferrate.Then,thevarianceformulaofthedatatransmissionratewasderived.Finally,therangesofazimuth,elevationangleanddistanceofISLintheWalker27/3/1constellationwereanalyzedbysimulation.Theimpactofdifferentcarrierfrequenciesanddataratesonthetransmissionpowerwerediscussed,andareasonabletransmissionpowerwasalsodetermined.
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Research on CO
2
Adsorption Characteristics of Hydrophobic ZSM-5 Adsorbent
WANG Xi-Qin, LI Kai, LUAN Zhi-Qiang, YE Ping-Wei
2012, 32 (
2
): 17-21. doi:
10.3780/j.issn.1000-758X.2012.02.003
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1958
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ThetraditionalCO
2
removalmethodwith 5A zeolite molecular sieve will lose efficacy because of the strong affinity with the water vapor.Ahydrophobic ZSM-5 adsorbent was preparedbyamixtureofZSM5,silicasol,waterandadditives,followedbyprocessesofextrusion,dryingandthenhydrophobicmodification.Thestructuresandpropertiesoftheadsorbentwere analyzed by N
2
, H
2
O/CO
2
adsorptionisothermsandXRDanalysismethods.Thepreparedadsorbenthasmultilevelpore structure,highBETspecificsurfacearea(296m
2
/g) andbetterCO
2
adsorptionperformance,aswell asexcellenthydrophobicity, and the H
2
O equilibriumadsorptioncapacityisabout1% of weightevenundertheconditionof90%relativehumidity.
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AbsoluteErrorSelectionCriteriaofUnconstrainedModefor FlexibleManipulatorDynamicsModelDimensionReduction
QI Nai-Ming, ZHAO Bao-Shan, ZHAO Zhi-Gang, WANG Li-Ping
2012, 32 (
2
): 22-28. doi:
10.3780/j.issn.1000-758X.2012.02.004
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1855
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Theunconstrainedmodedynamicsdimensionreductionmethodsonlyconsiderthestructuralparameterswithoutanalyzingtheimpactofthecontrolforce.DuetoanycontrolforcecanbeequivalenttothesuperpositionofaninfinitenumberofsinusoidalforcebyFourieranalysismethod,anunconstrainedmodeselectioncriteriaundersinusoidalforcebasedontheabsoluteerrorwaspresented.Theelasticdeformationofflexiblemanipulatorwasmodeledbyusingthefiniteelement(FE)method.ThedynamicsmodelofflexiblemanipulatorwasdeducedbyusingtheLagrangeapproach.Thesolutionofunconstrainedmodewasusedfordimensionreductionofthedynamicsequations.Thedimensionreductionofthedynamicsequationsandtheoriginaldynamicsequationswerecompared.Numericalsimulationsdemonstratethecorrectnessoftheproposedapproach.
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ConfigurationParameterAnalysisforADAM-typeArticulatedMast
LI Biao, LIU Zhi-Quan, CHENG Gang, DING Feng
2012, 32 (
2
): 29-34. doi:
10.3780/j.issn.1000-758X.2012.02.005
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2099
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TheconfigurationofADAM-typearticulatedmastwasdescribed,andmain configuration parameterswerechosen. FiniteelementmodelsoftheADAM-typemastwerebuiltupbyANSYS.Usingthesemodels,modeanalysiswascarriedout.By comparingtheanalysisresultswithexperimentresults,thecorrectnessofthefiniteelementmodelswasvalidated.Theeffectsofbaylength,canisterradius,crosssectionsideandpreloadofthediagonalcablesontheperformanceofthemastwereanalyzed.Theanalysisresultsshowthattheperformancecanbeimprovedbyincreasingthebaylength.Thebendingstiffnessandmassofthemastwillbepromotedasthecanisterradiusincreases.Thepreloadsofthediagonalcablesshouldbeselectedbetweentheallowableminimumvalueandthevaluecorrespondingtothesituationwhentheballsocketsobtainmaximumstiffness.Theseconclusionscouldbeappliedinmastengineeringdesign.
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Space Target Recognition Based on Improved Kernel FCM
WANG Xiao-Xue, YANG Yong-Sheng, JING Zhong-Liang
2012, 32 (
2
): 35-42. doi:
10.3780/j.issn.1000-758X.2012.02.006
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2238
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A recognitionsystemwaspresentedtoaccomplishspacetargetclassification.Firstly,Imagefeaturevectorswereextractedaccordingtoinvariantregionmoments,shapeandimagedescriptorsofspaceobjects.Andthen,clusteringalgorithmisappliedtotheclassifyspacetarget.AnimprovedkernelclusteringalgorithmbasedonVoronoidistancewasproposedwhichhadacrispermembershipfunctionandwasrobustfornoiseandoutliers.Experimentsshowthattheimprovedkernelfuzzyclusteringalgorithmismoreaccurateandvalidthanthatoftheconventionalmethods.
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StartupandOperatingCharacteristics ofCapillaryWickEvaporator
LI Jin-Wang, ZOU Yong, CHENG Lin
2012, 32 (
2
): 43-47. doi:
10.3780/j.issn.1000-758X.2012.02.007
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1923
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Theeffectsofporouswickporosityandheatsourcepoweronstartupand operatingcharacteristicsofcapillarywick evaporator(justlikealoopheatpipewithoutlinkingthevaporline)wasinvestigated.Theexperimentwascarriedoutwithout mixingtheeffectoftheworkingfluidandthecondenser.Theresultshowsthatthetemperatureoftheevaporatorwill fluctuateinsomecasesduringthestartupofthesystem.Theheatsourcepowerwhichmakesthetemperaturefluctuated decreasinglywiththeincreasingporosityoftheporouswick.Whenporouswickisthesame,temperatureiseasierto fluctuateanditwillbemuchseriouswith the biggerheatsourcepower.Thereasonforthetemperaturefluctuationisthatthe porosity of porous wick does notmatchwiththeoutsideparameters,suchastheheatcoursepower.
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ConvolutiveBlindSeparationAlgorithmBasedonSatelliteCommunicationAnti-jamming
WEN Yuan-Yuan, CHEN Hao
2012, 32 (
2
): 48-54. doi:
10.3780/j.issn.1000-758X.2012.02.008
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1783
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Aimingattheproblemofsatellitecommunicationsignalandjammingblindseparationinnoisyenvironment,anewalgorithmforconvolutivemixtureblindsourceseparation (BSS)byexploitingthehouseholdertransformationtorealizethejointdiagonalizationofhighordercumulantandoperationinthefrequencydomainwasproposed.Comparedwiththeclassicalmethods,simulationresultsshowthattheproposedalgorithmhaslowercomputationalcomplexityandbetterseparationperformance.Whensignal to noiseratio (SNR)isgreaterthan10dB,thenovelalgorithmofanti-jammingcanrealizetheseparationofcommunicationsignalsandthejamming,andhasgoodseparationperformance.
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MultipleFaultDiagnosisAlgorithmUnderLargeFalse-alarmRateTests
ZHANG Sen, YU Deng-Yun, WANG Jiu-Long
2012, 32 (
2
): 55-61. doi:
10.3780/j.issn.1000-758X.2012.02.009
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1932
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Multiplefaultdiagnosisunderunreliabletestsusingthemultisignalmodelwasstudied.TheoptimalmultiplefaultdiagnosisproblemisNPcomplete,sosuboptimalalgorithmwasusedforlargescalesystemdiagnosis.Agoodfaultestimationunderlowfalsepositiveratewasobtainedbythesubgradientoptimizationmethod.Butifthesizeofthegraphisbigandthefalsealarmrateishigh,thisalgorithmwill notbeabletoeliminatetheinfluenceoffalsepositive,andtheresultingestimationwouldcovereveryfailedtestinsteadoffindingthetruefaultpositionofthesystem.Anewkindofdiscriminatefunctionconsideringbothfalseandtruepositivetestswasused,andanimprovedgeneticalgorithmwasproposedtosearchthefailurecomponents.Simulationresultsshowthatthenewmethodisfasterthansubgradientoptimizationandhasahighercorrectisolationratewhenintercurrentfaultsarefew.
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Quasi-cycleLDPCConstructionMethod BasedonProtographExpansion
GONG Xian-Feng, TAO Xiao-Feng, QIU Le-De
2012, 32 (
2
): 62-67. doi:
10.3780/j.issn.1000-758X.2012.02.010
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2739
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Theperformanceoflowdensityparitycheckcode(LDPC)basedonprotopraphexpansiongreatlydependsontheexpansionmethod.AnewQC-LDPCconstructionmethodwasproposed.Twomainstepsintheparitycheckmatrixconstructionincludethemulti-edgeseliminationofprotographandquasi-cycleexpansion.Thefirststepmakelocalgirthmaximumundertheconstraintofedgepermutation.Inthesecondstep,optimumshiftvaluesofthepermutationmatriceswereobtainedbysearchingtheclosedloopswithinthespecifiedlengthandcomparingthelengthandapproximatecycleextrinsicmessagedegree(ACE)ofcycles,aimingatreducingsmallcycleswithlowconnectivitywhichwasharmfultothecodeperformance.Forprotographwithoutmulti-edges,theonlystepwasthequasicycleexpansion.Asprovedbysimulation,theconstructedQC-LDPChasexcellentperformanceinbothdecodingthresholdanderrorflooraspects.
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MultipleSpacecraftsOn-orbitServiceTaskAllocationBasedonDPSO
ZHANG Qi-Xin, SUN Fu-Chun, XU Bin, LIU Hua-Ping
2012, 32 (
2
): 68-76. doi:
10.3780/j.issn.1000-758X.2012.02.011
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Inordertosolvemulticonstrainedon-orbitservicetaskallocationforspacecraft,theprogrammingofon-orbitservicetaskallocationforon-orbitsatelliteswasstudied.Basedontheanalysisofthekeyfactorsincludingtargetsatellitevalue,servicespacecraftlossandenergy-timeconsumption,anon-orbitservicingmulti-spacecrafttaskallocationmodelwasformulated.Adiscreteparticleswarmoptimization (DPSO) algorithmwasproposedforon-orbitservicespacecraftcooperativetaskallocationproblems.Anewparticlepositionandnewupdatestrategyfortheparticlespeedweredeveloped.ThesimulationresultsshowthattheproposedDPSOalgorithmadmitsbetterconvergence,optimizationcapability,andcansolvetheon-orbitservicespacecraftcooperativetaskallocationeffectively.
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CoordinatedManeuverofSpacecraftFormationBasedonLine-of-sightMeasurement
ZHANG Wei, FENG Xiao-Hui, DENG Zhong-Min
2012, 32 (
2
): 77-83. doi:
10.3780/j.issn.1000-758X.2012.02.012
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1866
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Basedontheline-of-sightmeasurement,acooperativecontrolmethodforleaderlessformationflightispresented.Line-of-sightvectormeasurementisgeneratedwheneachsatelliteinaformationtracksitsneighboringspacecraft.Thefirstmemberoftheformationtracksthedesiredorbitaccordingtothecommandfromahighlevelcontroller.Achainformationisgenerated.Distancesbetweenline-of-sightmeasurementsaretakenasfeedbackoftheformationcontroller.Therelativeperturbationequationsareprovidedtomakesurethatmodelinguncertaintiesandperturbationsareconsideredinthecontrolstrategy.Cyclicformationcontrolisperformedviaslidingmodecontroller.Simulationresultsshowthattheproposedcontrolmethodcanbeusedforsatelliteformationmaintenanceandmaneuver.
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