›› 2015, Vol. 35 ›› Issue (1): 58-65.doi: 10.3780/j.issn.1000-758X.2015.01.008

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MissionProgrammingofPeer-to-PeerRefuelingonNon-CoplanarCircularOrbit

DUBingxiao,ZHAOYong,CHENLihu,YAOWen   

  1. (NationalUniversityofDefenseTechnology,  CollegeofAerospaceTechnologyandEngineering,Changsha410073)
  • Received:2014-08-28 Revised:2014-11-17 Online:2015-02-25 Published:2015-02-25

Abstract: TheaimoftheoptimalscheduleforthePeer-to-Peerrefuelingstrategyistofindthebestrendezvoustrajectorieswiththeminimumfuelconsumptionduringthewholemission.Firstly,themathematicmodelforthemissionprogrammingwassetup,whichwassummedupasathree-indexmatchproblem,andtheminimumfuelexpenditurewassettobetheobjective.Secondly,thealgorithmflowfortheproblemwasdesigned,andthecombinationofKuhn-Mundresalgorithmandtheintegergeneticalgorithmwereadopted,theconvergencewasacceleratedandtheglobaloptimizationwasguaranteed.Atlast,twoconstellationsinthenon-coplanarcircularorbitwithasmallintersectionanglewasconsideredasanexample,andtheoptimalschedulingandfuelcostfortwoimpulsemaneuverweregottensuccessfully.Andtheresultshowsthattheproposedmodelandalgorithmareefficient.

Key words: On-orbitrefueling, Tripartitegraph, Integergeneticalgorithm, Missionprogramming, Non-coplanarcircularorbit, Satellite