›› 2016, Vol. 36 ›› Issue (3): 57-62.doi: 10.16708/j.cnki.1000-758X.2016.0029
Previous Articles Next Articles
CAI Jian*, SONG Li-Fang, JIANG Qing-Hua
Received:
Revised:
Online:
Published:
Abstract: Thereislimitationtoconfirmingthereasonforthedatachangeofattitudesensorofspacecraftafterthetelemetrydatawerereceived,whichbringstheproblemthatthedatacan′tbeanalyzedintime.Tosolvethisproblem,anapproachwasproposedtostudytherangeofsolardisturbanceforattitudesensorbasedontwoangleparameterswhichreflectrelativepositionbetweenthesunandspacecraft.Therangeofsolardisturbanceforattitudesensorcouldgaininadvanceduetowellregulatedchangeofthetwoparameters.Consequently,whichcouldofferhelpfordatachangeandfailureanalysisofattitudesensor.Furthermore,itisbeneficialtothedesignofspacecraftattitudecontrolsystem,forexample,configurationandinstallationofattitudesensor.Inaddition,thefacultytorestrainsunlightofattitudesensorisvalidatedthroughtheway.Simulationresultsprovethevalidityofthealgorithm.
Key words: spacecraft, attitudesensor, solardisturbance, angleestimating, sunlightrestrain
CAI Jian, SONG Li-Fang, JIANG Qing-Hua. Anapproachtoanalyzetherangeofsolardisturbanceforattitudesensorofspacecraft[J]. , 2016, 36(3): 57-62.
0 / / Recommend
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: http://zgkj.cast.cn/EN/10.16708/j.cnki.1000-758X.2016.0029
http://zgkj.cast.cn/EN/Y2016/V36/I3/57