Chinese Space Science and Technology ›› 2013, Vol. 33 ›› Issue (6): 41-48.doi: 10.3780/j.issn.1000-758X.2013.06.006

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CombinedControlforQuickManeuverofElasticSatellite

 RAO  Wei-Dong1,2, XU  Li-Jia1,2   

  1. (1BeijingInstituteofControlEngineering,Beijing100190)
    (2ScienceandTechnologyonSpaceIntelligentControlLaboratory,Beijing100190)
  • Received:2013-01-04 Revised:2013-04-23 Published:2013-12-25 Online:2013-12-25

Abstract: Acombinedcontrolmethodwhichconsistsoffeedbackcontrolandfeedforwardcontrolwaspresented.Thefeedbackloopeliminatesrigidbody′sattitudeerroraroundtargetattitude,whilefeedforwardcontrolpreventsfromelasticvibration.Forfeedbackloop,thetraditionalPDcontrolwasadopted.Forfeedforwardcontrol,thesuboptimalsinusoidalcontrolwasadopted.Suboptimalsinusoidalcontrolconsistsofseriesofsinusoidsexcitinglittlevibrationofelasticmodesfromlowordertohighorder.Numericalsimulationwascarriedouttoverifythemethod.Theresultsshowthat,byusingthecombinedcontrol,themaneuvertaskcanbefulfilledeffectivelyinthepresenceofdynamicaluncertaintiesanddisturbance.

Key words: Quickmaneuver, Combinedcontrol, Suboptimalsinusoidalcontrol, Gausspseudospectralmethod, Elasticsatellite