Vision-BasedRelativeNavigationforRendezvousandDockingofSpacecraft

doi:10.3780/j.issn.1000-758X.2013.06.005

Chinese Space Science and Technology ›› 2013, Vol. 33 ›› Issue (6): 33-40.doi: 10.3780/j.issn.1000-758X.2013.06.005

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Vision-BasedRelativeNavigationforRendezvousandDockingofSpacecraft

LIU Yong¹, XU Peng¹, XU Shi-Jie2

(1BeijingInstituteofSpacecraftSystemEngineering,Beijing100094)
(2BeihangUniversity,Beijing100191)

Received:2012-09-11 Revised:2013-07-08 Published:2013-12-25 Online:2013-12-25

Abstract

Abstract: Forthefinalphaseofspacecraftautonomousrendezvousanddocking,thevisionrelativenavigationmethodbasedontheinformationofthespecificreferencelightsourceswaspresented.Undertheassumptionofsmallattitudeangle,therelativenavigationmodelswerededuced.Theclosed-formsolutionforrelativeattitudeandpositionparametersbasedonthevisionnavigationmodelswasderived.ThereducedorderUnscentedKalmanFiltering(UKF)algorithmwasdesignedtoestimatetheinformationofrelativeattitudeangleandrelativeattitudeanglevelocity.Simulationresultsshowthattheproposedapproachprovidesaconvenientwayforobtainingtheinformationofrelativepositionandrelativeattitude,andthereducedorderUKFcanimprovetheaccuracyoftherelativeattitudedetermination.

Key words: Autonomousrendezvousanddocking, Visionbasedrelativenavigation, Relativeattitudedetermination, Spacecraft

LIU Yong, XU Peng, XU Shi-Jie. Vision-BasedRelativeNavigationforRendezvousandDockingofSpacecraft[J]. Chinese Space Science and Technology, 2013, 33(6): 33-40.

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Vision-BasedRelativeNavigationforRendezvousandDockingofSpacecraft

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