ConfigurationParameterAnalysisforADAM-typeArticulatedMast

doi:10.3780/j.issn.1000-758X.2012.02.005

Abstract

Abstract: TheconfigurationofADAM-typearticulatedmastwasdescribed,andmain configuration parameterswerechosen. FiniteelementmodelsoftheADAM-typemastwerebuiltupbyANSYS.Usingthesemodels,modeanalysiswascarriedout.By comparingtheanalysisresultswithexperimentresults,thecorrectnessofthefiniteelementmodelswasvalidated.Theeffectsofbaylength,canisterradius,crosssectionsideandpreloadofthediagonalcablesontheperformanceofthemastwereanalyzed.Theanalysisresultsshowthattheperformancecanbeimprovedbyincreasingthebaylength.Thebendingstiffnessandmassofthemastwillbepromotedasthecanisterradiusincreases.Thepreloadsofthediagonalcablesshouldbeselectedbetweentheallowableminimumvalueandthevaluecorrespondingtothesituationwhentheballsocketsobtainmaximumstiffness.Theseconclusionscouldbeappliedinmastengineeringdesign.

Key words: Able deployable articulated mast, Deployable mechanism, Configuration, Finite element method, Parameter analysis, Spacecraft

LI Biao, LIU Zhi-Quan, CHENG Gang, DING Feng. ConfigurationParameterAnalysisforADAM-typeArticulatedMast[J]. Chinese Space Science and Technology, 2012, 32(2): 29-34.

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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2012.02.005

https://journal26.magtechjournal.com/kjkxjs/EN/Y2012/V32/I2/29

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ConfigurationParameterAnalysisforADAM-typeArticulatedMast

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