Anapproachtoanalyzetherangeofsolardisturbanceforattitudesensorofspacecraft

doi:10.16708/j.cnki.1000-758X.2016.0029

Abstract

Abstract: Thereislimitationtoconfirmingthereasonforthedatachangeofattitudesensorofspacecraftafterthetelemetrydatawerereceived,whichbringstheproblemthatthedatacan′tbeanalyzedintime.Tosolvethisproblem,anapproachwasproposedtostudytherangeofsolardisturbanceforattitudesensorbasedontwoangleparameterswhichreflectrelativepositionbetweenthesunandspacecraft.Therangeofsolardisturbanceforattitudesensorcouldgaininadvanceduetowellregulatedchangeofthetwoparameters.Consequently,whichcouldofferhelpfordatachangeandfailureanalysisofattitudesensor.Furthermore,itisbeneficialtothedesignofspacecraftattitudecontrolsystem,forexample,configurationandinstallationofattitudesensor.Inaddition,thefacultytorestrainsunlightofattitudesensorisvalidatedthroughtheway.Simulationresultsprovethevalidityofthealgorithm.

Key words: spacecraft, attitudesensor, solardisturbance, angleestimating, sunlightrestrain

CAI Jian, SONG Li-Fang, JIANG Qing-Hua. Anapproachtoanalyzetherangeofsolardisturbanceforattitudesensorofspacecraft[J]. Chinese Space Science and Technology, 2016, 36(3): 57-62.

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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.16708/j.cnki.1000-758X.2016.0029

https://journal26.magtechjournal.com/kjkxjs/EN/Y2016/V36/I3/57

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Anapproachtoanalyzetherangeofsolardisturbanceforattitudesensorofspacecraft

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