ImprovedHaloOrbitControlMethodBasedonPoleAssignment

doi:10.3780/j.issn.1000-758X.2012.05.008

Chinese Space Science and Technology ›› 2012, Vol. 32 ›› Issue (5): 47-53.doi: 10.3780/j.issn.1000-758X.2012.05.008

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ImprovedHaloOrbitControlMethodBasedonPoleAssignment

CHAO Ning¹, LUO Xiao-Ying², LI Yan-Jun¹

(1InstituteofAstronomy,NorthwesternPolytechnicalUniversity,Xi′an710072)
(2Xi′anPowerElectronicResearchInstitute,Xi′an710061)

Received:2011-12-22 Revised:2012-02-27 Published:2012-10-25 Online:2012-10-25

Abstract

Abstract: Basedonsmalldeviationtheory,theno-perturbation3-bodydynamicequationswerelinearizedandtheerrorlinearmodelwas deduced.Basedonthepoleassignmenttheoryoflinearsystem,stationkeepingforperturbedhaloorbitnearL₁pointinEarth-MoonsystemwasachievedthroughdesigningtheclosedlooppoleassignmentstatefeedbackmatrixKbychoosing standardorbitstatevectorasclosedlooptargetpole.Aimedatthecontrolerrorcausedbysinglecontrollevelofthreeaxis in K ,adesignmethodofvariablefeedbackmatrixKcoefficient(VKC)consideringthescaleoforbitinjectionwasproposed.TheexperimentsshowthattheVKCmethodwhichimprovedcontroleffectoforiginalcontrolmethodanddecreasedtrackingvariancesumunderdifferenterrorlevelsisavailable.

Key words: Haloorbit, Librationpoint, Poleassignment, Orbitstationkeeping, Spacecraft

CHAO Ning, LUO Xiao-Ying, LI Yan-Jun. ImprovedHaloOrbitControlMethodBasedonPoleAssignment[J]. Chinese Space Science and Technology, 2012, 32(5): 47-53.

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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2012.05.008

https://journal26.magtechjournal.com/kjkxjs/EN/Y2012/V32/I5/47

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ImprovedHaloOrbitControlMethodBasedonPoleAssignment

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