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230027QuadrotorHelicopter。PID。。PIDV271.4A1671-637X201203-0051-05DesignofaQuadrotorHelicopterandItsSmoothMotionControlSimulationPANGQingpeiLIJiawenHUANGWenhaoDepartmentofPrecisionMachineryandPrecisionInstrumentationUniversityofScienceandTechnologyofChinaHefei230027ChinaAbstractThebroadapplicationrequirementofquadrotorhelicoptersinbothmilitaryandcivilianmarketsduetotheiradvantagesoverregularairvehiclesstimulatesthedevelopmentofthem.AquadrotorhelicopterwasdesignedandfabricatedwithKalmanfilterusedforattitudecalculationandPIDcontrolutilizedforattitudecontrol.Dynamicalmodelswereestablishedforthequadrotorhelicopteranditspowersystem.Theresultsofsimulationandflighttestshowedthattheproposedcontrolstrategyisfeasibleandtheeffectivenessofthedynamicmodelswasverified.KeywordsquadrotorhelicoptermodelingKalmanfilterPID0、、。、、、1。MEMSMicroElectroMechanicalSys-tems。。VTOL、、、2011-02-132011-05-111984—。。。2。。1。Euler-Lagrange2。。3Euler、θψ。1。。19320123ElectronicsOptics&ControlVol.19No.3Mar.20121Fig.1Definitionofthecoordinateframes1.1、。L·didt=u-Rmi-Ceωm1Jm·dωmdt+fmωm=Mm-MloadJm·dωmdt+fmωm=Mm-Mload2JmωmMmMloadfmuiCeCeωm。Mm=CmiCmMm。Jm·dωmdt=-C2mRm·ωm-Mc+CmRm·u3。Mc=dω2propellor=dω2md。1.2Eulerθψpqr。。pqr=10-sinθ0cossincosθ0-sincossinθ·θ·ψ·4L=T-VΓi=ddtLq·()i-Lq{i5Lqiq·iΓi。Ixx¨=θ·ψ·Iyy-IzzIyyθ¨=·ψ·Izz-IxxIzzψ¨=·θ·Ixx-Iyy{63。3RxxRyθyRzψz。Rθψ=RxRyθRzψ7XY[]Zxy[]zrXYZxyz=Rθψ()xyzT8。、、Ixx¨=θ·ψ·Iyy-Izz-Jθ·Ωsum+MxpropIyyθ¨=·ψ·Izz-Ixx+J·Ωsum+MypropIzzψ¨=·θ·Ixx-Iyy+MzpropΩsum=-Ω1-Ω2+Ω3+Ω49IxxyyzzθψoxzoyzIxyzyxz=0。MsumthrustMxprop34Myprop12Mzprop12343。Msumthrust=blΩ21+Ω22+Ω23+Ω24Mxprop=blΩ24-Ω23Myprop=blΩ22-Ω21Mzprop=dΩ21-Ω23+Ω22-Ω2410Mxprop'=JrωyΩ1+Ω2-Ω3-Ω4Myprop'=JrωxΩ3+Ω4-Ω1-Ω2{11JrΩ。xyz2519Mxpropsum=blΩ24-Ω23+JrωyΩ1+Ω2-Ω3-Ω4Mypropsum=blΩ22-Ω21+JrωxΩ3+Ω4-Ω1-Ω2Mzpropsum=dΩ21-Ω23+Ω22-Ω24{12、。21.1kg125cm。。4。4。。InertialMeasurementUnitIMU。2.1。IMU3ADXRS300MMA7260QT。2.2。PPMPulsePositionModulation。2.3FT06-ALM393G1PPMPulsePositionModulationSumSignal。2.4、。、、、、、、。。2.5。ATMEGA644P。I2C4。3C。PID。3.15。6。。yK。7。1u=gyro_rate132x=A·x+B·u143y=acc_angle154Inn=y-C·x165S=C·P·CT+SZ176K=A·P·CT·S-1187353x=x+K·Inn198P=A·P·AT-K·C·P·AT+SW201。。53。。1Table1ListofsymbolsA1.0-0.020.01.0B0.020.0C1.00.0SZ17.2SW0.0050.0050.0050.005P0.0050.0050.0050.0053.2PID。。EurocopterTigerPID。。PIPI。PI。I。IPI。PIPI。4MatlabSimulink。。0°。48。4PWM。122-8°9°3-11°15°。2Table2ListofparametersM1.1kgl0.625mJx0.10327kg·m2Jy0.10327kg·m2Jz0.25358kg·m22Fig.2Simulationresultswithoutanydisturbances3Fig.3Simulationresultsunderdisturbances4。60s20°。IMU。45194Fig.4Theflighttest5PIDMatlabSimulink。、、。1BOUABDALLAHSBECKERMSIEGWARTR.Autono-mousminiatureflyingrobotsComingsoonJ.IEEERobotics&AutomationMagazine200714388-98.2BOUABDALLAHSSIEGWARTR.DesignandcontrolofquadrotorswithapplicationtoautonomousflyingD.EP-FL2006.3BOUABDALLAHSSIEGWARTR.Fullcontrolofaquadro-torC//2007IEEE/RSJInternationalConferenceonIn-telligentRobotsandSystemsVOLS.2007153-158.4.J.2007146113-117.5LEFFERTSEJMARKLEYFLSHUSTERMD.KalmanfilteringforspacecraftattitudeestimationJ.JournalofGuidanceControlandDynamics198255417-429.6CRASSIDISJLMARKLEYFLCHENGY.SurveyofnonlinearattitudeestimationmethodsJ.Journalofguidancecontrolanddynamics200730112-28.7.Matlab6.xKal-manJ.20041869-71.8MIANAAWANGDB.NonlinearflightcontrolstrategyforanunderactuatedquadrotorC//AerialRobot2008IEEEInternationalConferenceonNetworkingSensingandControl.SanyaChina2008938-942.39。1.SIFTJ.200730610-12.2.SIFTJ.200932650-53.3LOWEDG.DistinctiveimagefeaturesfromscaleinvariantkeypointsJ.InternationalJournalofComputerVision200460291-110.4LOWEDG.Localfeatureviewclusteringfor3DobjectrecognitionC//IEEEConferenceonComputerVisionandPatternRecognition2001682-688.5LOWEDG.Objectrecognitionfromlocalscale-invariantfeaturesC//InternationalConferenceonComputerVision19991150-1157.6LOWEDG.Fittingparameterizedthree-dimensionalmodelstoimagesJ.IEEETrans.PatternAnalysisandMachineIn-telligence1991135441-450.7MIKOLAJCZYKKSCHMIDC.AperformanceevaluationoflocaldescriptorsJ.IEEETransPatternAnalysisandMachineIntelligence200527101615-1630.8SUKTHANKARR.PCA-SIFTAmoredistinctiverepre-sentationforlocalimagedescriptorsC//ProceedingsConferenceComputerVisionandPatternRecognition2004511-517.9DELPONTEELSGROFODONEFetal.SVD-matchingusingSIFTfeaturesJ.GraphicalModels2006685415-431.10.SIFTJ.2008371181-183.11.SIFTJ.201022112760-2763.12.SIFTJ.200934101245-1249.553
本文标题:四旋翼飞行器设计与平稳控制仿真研究
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