Chinese Space Science and Technology ›› 2015, Vol. 35 ›› Issue (6): 20-.doi: 10.3780/j.issn.1000-758X.2015.06.003
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WANG Yi-Ping, ZHAO Yu-Shan, SHI Peng, ZHENG Han-Qing
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Abstract: Anadaptivecontrolbasedondynamicsmodelforstabilizingthecouplingsystemwasproposed,forthecouplingsystemmaybeunstableduetothechangeinmasscharacteristicsandmomentumofthecouplingsystem.Thedynamicsofsystemwasmodelledandthevelocitiesofcouplingsystemwerederivedfromtheimpactmodel.Basedonthedynamicmodeldeveloped,thelinearfeedbackcontrollerwasdesigned.Becauseoftheuncertaintyonthedynamicparametersanddisturbance,thedynamicmodelwaslinearlyparametricwithrespecttoagroupofunknowndynamicparametersandunknowndisturbance.Then,theadaptivelinearfeedbackcontrollerwasdesigned.UsingathreeDOFplanarspacemanipulator,thenumericalsimulationwascarriedout.Thesimulationresultsconfirmthecontrollerisfeasibleandeffective.
Key words: Couplingsystem, ImpactdynamicsDisturbanceLinearization;Adaptivecontrol;InorbitcaptureSpacemanipulator
WANG Yi-Ping, ZHAO Yu-Shan, SHI Peng, ZHENG Han-Qing. AdaptiveControlforStabilizingtheCouplingSystemwithDisturbanceafterCapturingSpacecraft[J]. Chinese Space Science and Technology, 2015, 35(6): 20-.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2015.06.003
https://journal26.magtechjournal.com/kjkxjs/EN/Y2015/V35/I6/20