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中国空间科学技术
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25 December 2016, Volume 36 Issue 6
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Review of reentry guidance methods for hypersonic gliding vehicles
LIU Si-Yuan, LIANG Zi-Xuan, REN Zhang, LI Qing-Dong
2016, 36 (
6
): 1-13. doi:
10.16708/j.cnki.1000-758X.2016.0066
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1032
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Thedevelopmentofreentryguidancemethodsforhypersonicglidingvehicleswasreviewed.Firstly,thedynamicsofareentryvehiclewasestablished.Thepathconstraints,theterminalconstraintsandthegeographicconstraintswereanalyzedforareentryflight.Secondly,longitudinalreentryguidancealgorithmsweredividedintothreecategories:thetrajectorytrackingmethod,thepredictorcorrectormethod,andthehybridmethod.Lateralreentryguidancealgorithmsweredividedintotwocategories:guidancefortheconventionalconstraintsandguidanceforthegeographicconstraints.Reviewswerepresentedforthethreelongitudinalguidancemethodsandthetwolateralguidancemethods.Finally,theguidancetechnologywasprospectedforhypersonicglidingvehiclesaccordingtoflightmissionsinthefuture.
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Deploymentstrategyoptimizationofonorbitservicingsystemforrefuelinggeosynchronousorbitsatellites
MENG Bo, XU Sheng, HUANG Jian-Bin, LI Zhi, PANG Yu-Jia, HAN Xu
2016, 36 (
6
): 14-21. doi:
10.16708/j.cnki.1000-758X.2016.0067
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Prolonglifespanofgeosynchronousorbit(GEO)satellitesbyrefuelingsatellitesonorbithaseconomicvalue.Asaresult,itisveryimportanttoassesstheon-orbitservicing(OOS)paradigmandoptimizeitsutilities.TheassessmentofOOSsystemforrefuelinggeosynchronoussatellitesandoptimizationmethodsofitsdeploymentstrategywerestudied.AnewarchitectureofOOSsystemwasproposed,whichincludedafuelstoragestationand
N
refuelingspacecraft(1+
N
).Thefuelstoragestationcarriedagreatdealoffuel,runningonorbitsteadily.TherefuelingspacecraftmaneuveredongeosynchronousorbitandimplementedtherefuelingmissionforGEOsatellites,whenthespacecraftransoutoffuel,itcametothestationandacquiredfuel.Theweightandorbitoffuelstoragestation,thenumber,weightandorbitofrefuelingspacecraftwerethekeyproblemsofdeploymentstrategy.ThemathematicmodelofoptimizationofthedeploymentstrategywhichshortentheresponsetimeofrefuelingGEOsatellitesandlowerthepriceofservicingsystemasmulti-objectiveswasconstructed.Thecalculationprocessoftheoptimizationwasanalyzed.Byanalyzingtheoptimizationresults,theoptimaldeploymentstrategyofservicingsystemcontainingafuelstoragestationand4-6refuelingspacecraftusedforrefuelingGEOsatelliteswasproposed.
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ResearchonspacebornevideoSARsystemdesignandimageformationalgorithm
LIANG Jian, ZHANG Run-Ning, BAO Min-Feng
2016, 36 (
6
): 22-28. doi:
10.16708/j.cnki.1000-758X.2016.0068
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954
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Asanewmicrowaveremotesensingmode,avideoSARcanprovideacontinuoussurveillanceoveraregionofinterest.ResearchesaboutspacebornevideoSARwerelimited.MostofcurrentresearchesaboutvideoSARonlyfocusonaircraftplatform.AspacebornevideoSARsystemwasdevelopedwiththetransmitterongeostationarysatellitesandthereceiveronthelowearthorbit(LEO)satellites.Therelationshipbetweentheimagingperformanceandthemainsystemparametershasbeenstudied.Thenanimageformationalgorithmwaspresented,whichcouldsatisfytheimagingqualityofvideoSARinhighsquintmodeandavoidunnecessaryduplicationofprocessing.TheDopplersmearandoffsetofthemovingtargetswerereflectedbytheprocessedimages.Meanwhile,thestationarytargetscanbefinelyfocusedon.
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Amissionplanningmethodfordeepspaceexplorerconsideringdynamicuncertainties
WANG Xiao-Hui, LI Shuang
2016, 36 (
6
): 29-37. doi:
10.16708/j.cnki.1000-758X.2016.0069
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784
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Anewmissionplanningalgorithmwasproposedtodealwiththeproblemsoflowidentifiabilityofdynamicuncertaintiesandsinglenessofresponsestrategyintraditionalmissionplanningalgorithmsfordeepspaceexplorer.Firstly,thelevelofdisturbancegeneratedbydynamicuncertaintieswasdividedintofourlevels.Fuzzyneuralnetworkwasusedtoevaluatethelevelofuncertainties,anditcanhelptochoosetheappropriateresponsestrategy.Secondly,alocalmissionrepairplanningmethodbasedonhierarchicaltasknetwork(HTN)wasproposedtoredecomposetheinvalidcomplexmissionscausedbythedisturbanceofuncertaintieswhentheresponsestrategywasrepairplanningstrategy.Finally,computersimulationresultsshowthattheproposedalgorithmcaneffectivelyevaluateandrespondtodeepspacedynamicuncertainfactors,andthereforeimprovethereliabilityandflexibilityofthemissionplanningalgorithm.
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Segmentationofhigh-resolutionmulti-spectralremotesensingimagebasedonmulti-feature
JIN Yong-Tao, LI Xu-Qing, ZHANG Zhou-Wei, CHEN Xi
2016, 36 (
6
): 38-46. doi:
10.16708/j.cnki.1000-758X.2016.0070
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892
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Aimingattheproblemthatthetraditionalimagesegmentationalgorithmscannotbeappliedtohighresolutionremotesensingimageswithmanyfeatures(spectral,textureandgeometricfeatures),aremotesensingimagesegmentationmethodbasedonmulti-featurewasproposed.Thealgorithmintegratedtheimprovedmeanshiftfilteringandautomaticmarkerwatershedtoachievethesegmentationperformance.Firstly,anautomaticmarkerwatershedmethodwasusedtosegmenttheremotesensingimageforextractinggeometricfeatureusingaffinemomentinvariantsofshapeoperator.Secondly,agraylevelco-occurrencematrixofthefirstprincipalcomponentwascalculatedastexturalfeature.Thirdly,multi-featurefilteringresultswereobtainedbyusingimprovedmeanshiftalgorithmincludingspectralfeature.Finally,thefilteringresultswereperformedusingtheautomaticmarkerwatershedsegmentationmethod.Inordertoshowtheeffectoftheproposedmethod,anunsupervisedevaluationandcomparisonoftheimagesegmentationfromtheproposedalgorithmandsinglewatershedsegmentationwereimplementedusingmulti-spectralinformationentropy.Theexperimentalsegmentationresultsshowthattheproposedalgorithmcanreducetheover-segmentationphenomenonefficientlyanditissuitedforthesegmentationofhigh-resolutionmulti-spectralremotesensingimage.
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Anadaptedgeneticalgorithmappliedtosatelliteautonomoustaskscheduling
ZHAO Ping, CHEN Zhi-Ming
2016, 36 (
6
): 47-54. doi:
10.16708/j.cnki.1000-758X.2016.0064
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848
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Aimingatsolvingtheproblemofautonomoustaskschedulingofearthobservingsatelliteswiththeabilityofswinging,satelliteautonomoustaskschedulingproblemandconstraintsweredescribed.Asingle-objectivemulti-constraintsmodelwasbuiltaccordingtotheNP-hardcharacterofsatelliteautonomoustaskschedulingproblem.Anadaptedgeneticalgorithmwasdesigned.Allofthegeneticoperationsofgeneticalgorithmswereoptimized.Firstly,mini-regionmethodwasappliedtogenerateoftheoriginalpopulationtoensurethediversityofpopulation.Adaptiveprobabilitieswereusedforcrossoverandmutationoperation.Twogenerationscompetitivetechnologywasusedtoavoidtheprematureandimprovetheefficiencyandtherobustnessofthealgorithm.Thealgorithmalsousestheoptimizationreservedstrategytopreservetheoptimalsolution,whichmakesthealgorithmconvergetotheglobal.Theadaptedgeneticalgorithmwasappliedtothelocalmulti-conflicttasksobservationanddesignedsimulationexperimentsoftheobservationofregionaldensetargets.Theresultsarecomparedwithresultsofsimulatedannealingalgorithmandimmuneantcolonygeneticalgorithm,anditshowsthattheproposedalgorithmismoreeffectiveandithasabetterconvergence.
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Rapidthermaldeformationanalysisofon-orbitsatellitesonthebasisofstatisticmethod
ZHANG Ye-Chi, ZHANG Long, LUO Wen-Bo, PAN Teng
2016, 36 (
6
): 55-61. doi:
10.16708/j.cnki.1000-758X.2016.0062
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722
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Tocalibratetheorientationpositionofthesatelliteorbitbythetemperaturesensors,theordinaryKrigingmethodwidelyusedingeo-statisticswasappliedintothetemperatureestimationprocessofthesatellite.Arapidthermaldeformationanalysismethodwasdevelopedbasedonthestatisticmethods.Basedonasmallamountoftemperaturesensors,estimationofthetemperaturefieldwascarriedout.Then,thetemperaturefieldwasusedforthefiniteelementanalysistoaccomplishthethermaldeformationanalysis.Differencesbetweentheanalyticalandtheexperimentalresultsofthedeformationofthepayloadarearound1′,whichconfirmsthatthemethodcanbeusedtoobtainthevariationofopticalaxisofthepayload.Furthermore,comparedtothethermophysicalmethod,theworkperiodcanbereducedbyseveraldays.Thisworkprovidesguidanceforrapidthermaldeformationanalysisofon-orbitsatellites.
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Apre-emptiblereal-timeSpaceWireon-boardnetwork
WU Zhong-Jie, LIU Jiang-Lan, SONG Wei, YU Jun-Jie, LIN Jing-Ming, ZHAO Zhan-Feng
2016, 36 (
6
): 62-69. doi:
10.16708/j.cnki.1000-758X.2016.0063
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753
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Tobuildunifiedon-boardcommunicationinfrastructurebasedonSpaceWrie,researchshouldbedonetoguaranteethedeterministicandreal-timeperformanceofmessagetransmission.Toovercomethelackofflexibilityintraditionaltime-triggeredcommunication,amodifiedtime-triggeredSpaceWirenetworkwhichsupportedthebroadcastingofcommunicationtasktransmissionidentifierwasproposed.Onthisbasis,anon-destructivepre-emptiblecommunicationmechanismwasbuiltandtheapplicationofclassicalprocessorreal-timeschedulingalgorithmtocommunicationtaskschedulingwasdiscussed.Atlast,thetransmissiondelayperformancewasanalyzedandcomparedamongevent-triggered,traditionaltime-triggeredandnon-blockingreal-timeSpaceWirecommunicationmechanisms.Theresearchshowsthatthiscommunicationmechanismcanreducetheworst-caseend-to-enddelay,andissuitedfortheschedulingofcommunicationtaskswithvariouspriorities.
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Multi-satelliteseparationsimulationbasedonvirtualprototype
WANG Jin-Chang, YAN Bo, ZHANG Jia, LI Cheng-Xiang, ZHANG Yao-Lei
2016, 36 (
6
): 70-76. doi:
10.16708/j.cnki.1000-758X.2016.0065
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782
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Inmulti-satellitelaunchmission,thesatelliteseparationsimulationisrelativelycomplicated.Themotionstateisinfluencedbymultiplefactors,includingseparationspringforce,explosiveboltimpact,electricalconnectortension,spacecraftmass-property,initialmotionalparametersandsoon.Itisdifficulttosolvebyusingthetraditionalnumericalcalculationmethod.Virtualprototypingtechnologyisaneffectivewaytosolvetheproblemsabove.Thesatelliteseparationanalysiswascompletedbyvirtualprototypetechnology,throughsettingdeviationandinterference,simulatedthesatellitesseparationprocessunderthedeviationandfaultmode,evaluatedthepossibilityofcollisionandotherdangerousoccurrence.Theresultsshowthattheimpactontheseparationresultsfromsystemdeviationcanbeevaluatedbysimulation,springselectionisneededinthecaseofhighrisk.Secondary,theinterferencecausedbyelectricalconnectorsgenerallydoesnotaffecttheseparationsafetyduetotheshortactiontime.
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Realtimeschedulingbasedontimetriggered1553Bbus
ZHAN Pan-Pan, GUO Jian, LIU Xin
2016, 36 (
6
): 77-82. doi:
10.16708/j.cnki.1000-758X.2016.0071
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769
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Inordertooptimizetheperformanceof1553Bbustransmission,reducethewaitingtimeafterthemessagestransmission,andimprovethebusbandwidthutilizationandtherealtimeperformanceofemergencymessagesresponse,the1553Bbusschedulingmethodswerestudied,andarealtimeschedulingmethodbasedonthetimetriggered1553Bbuswasdesignedbyusingthemethodofperiodicschedulingandpreemptivescheduling.Onthebasisoftimetrigger,busmessageswerecentrallyscheduledbypriority.Duringthetimethebusframewastransmittedonthebus,theprocessorcouldcontinueprocessingothertaskswithoutwaitingforsometime.Basedonthecharacteristicofbusdataareapartition,thepreemptiveschedulingstrategyforemergencymessagestointerruptcommonmessagestransmissionwasdesigned.Nonimportantdatadidn′ttakeupthebuschannelforalongtime,sothatemergencymessageswerequicklyresponded.Theexperimentalresultsshowthattheproposedmethodcanachievethemaximumcapacityofbustransmission.Itcanimprovethetransmissionefficiencyandbandwidthutilizationof1553Bbus,whiletheresponsetimeofemergencymessagesisstablewithin2ms.
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