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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RAO Wei-Dong1,2, XU Li-Jia1,2
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Abstract: Acombinedcontrolmethodwhichconsistsoffeedbackcontrolandfeedforwardcontrolwaspresented.Thefeedbackloopeliminatesrigidbody′sattitudeerroraroundtargetattitude,whilefeedforwardcontrolpreventsfromelasticvibration.Forfeedbackloop,thetraditionalPDcontrolwasadopted.Forfeedforwardcontrol,thesuboptimalsinusoidalcontrolwasadopted.Suboptimalsinusoidalcontrolconsistsofseriesofsinusoidsexcitinglittlevibrationofelasticmodesfromlowordertohighorder.Numericalsimulationwascarriedouttoverifythemethod.Theresultsshowthat,byusingthecombinedcontrol,themaneuvertaskcanbefulfilledeffectivelyinthepresenceofdynamicaluncertaintiesanddisturbance.
Key words: Quickmaneuver, Combinedcontrol, Suboptimalsinusoidalcontrol, Gausspseudospectralmethod, Elasticsatellite
RAO Wei-Dong, XU Li-Jia. CombinedControlforQuickManeuverofElasticSatellite[J]. Chinese Space Science and Technology, 2013, 33(6): 41-48.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2013.06.006
https://journal26.magtechjournal.com/kjkxjs/EN/Y2013/V33/I6/41