Control System Development and Flight Test Experience with theMQ-8B Fire Scout Vertical Take-Off Unmanned Aerial Vehicle (VTUAV) 控制系统开发与飞行试验经验 MQ-8B型火控侦察机垂直起飞无人机

Control System Development and Flight Test Experience with theMQ-8B Fire Scout Vertical Take-Off Unmanned Aerial Vehicle (VTUAV) 控制系统开发与飞行试验经验 MQ-8B型火控侦察机垂直起飞无人机

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时间:2019-08-08

Control System Development and Flight Test Experience with theMQ-8B Fire Scout Vertical Take-Off Unmanned Aerial Vehicle (VTUAV) 控制系统开发与飞行试验经验 MQ-8B型火控侦察机垂直起飞无人机_第1页
Control System Development and Flight Test Experience with theMQ-8B Fire Scout Vertical Take-Off Unmanned Aerial Vehicle (VTUAV) 控制系统开发与飞行试验经验 MQ-8B型火控侦察机垂直起飞无人机_第2页
Control System Development and Flight Test Experience with theMQ-8B Fire Scout Vertical Take-Off Unmanned Aerial Vehicle (VTUAV) 控制系统开发与飞行试验经验 MQ-8B型火控侦察机垂直起飞无人机_第3页
Control System Development and Flight Test Experience with theMQ-8B Fire Scout Vertical Take-Off Unmanned Aerial Vehicle (VTUAV) 控制系统开发与飞行试验经验 MQ-8B型火控侦察机垂直起飞无人机_第4页
Control System Development and Flight Test Experience with theMQ-8B Fire Scout Vertical Take-Off Unmanned Aerial Vehicle (VTUAV) 控制系统开发与飞行试验经验 MQ-8B型火控侦察机垂直起飞无人机_第5页
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1、ControlSystemDevelopmentandFlightTestExperiencewiththeMQ-8BFireScoutVerticalTake-OffUnmannedAerialVehicle(VTUAV)JamesDownsRonPrenticeScottDalzellAdamBesachiojames.downs@ngc.comron.prentice@ngc.comscott.dalzell@ngc.comadam.besachio@ngc.comGNCEngineerGNCEngineerGNCEngineerGNCEngineerIntegratedSystems,

2、UnmannedSystemsNorthropGrummanCorporation,RanchoBernardo,CAChristinaM.IvlerMarkB.TischlerMohammadrezaHosseinMansurCIvler@mail.arc.nasa.govMTischler@mail.arc.nasa.govHMansur@mail.arc.nasa.govResearchEngineer,SanJoseSeniorScientistAerospaceEngineerStateUniversityFoundationFlightControlGroupLeaderAerof

3、lightdynamicsDirectorate(AMRDEC)U.S.ArmyResearch,Development,andEngineeringCommand,MoffettField,CAAbstractThispaperdescribesthecontrolsystemdevelopmentoftheMQ-8BFireScoutautonomoushelicopter.Itincludesadiscussionofthesystemidentificationprocessandsomedetailsonimplementingtheidentificationoutputintoa

4、sixdegreeoffreedomsimulation.Innerloopcontrollawsynthesisusingclassical,andtwodifferentmoderndesigntoolsformeetingspecificstabilityandperformancemetricsisalsopresented.Thisisfollowedbythedetailsoftheclassicalouterloopdesignprocess.Finally,somepreliminaryflighttestresultsarepresentedfromthesuccessful

5、initialflights.NOMENCLATUREOGE:OutofgroundeffectP5:Prototype5Acronyms:UAV:UnmannedAirVehicleVTUAV:VerticalTake-offUnmannedAirVehicleAFDD:U.S.ArmyAeroflightdynamicsDirectorate®CIFER:ComprehensiveIdentificationfromFrequencySymbolsResponses®MStatederivativematrixCONDUIT:ControlDesigner’sUnifiedInterfac

6、eFStatematrixCRDA:CooperativeResearchandDevelopmentGControlmatrixAgreementHOutputstatematrixDARPA:DefenseAdvancedResearchProjectsAgencyLDerivativeforspecificrollingmomentEMD:EngineeringManufacturingDesignMDerivativeforspecificpitchingmomentGNC:GuidanceNavigationandControlNDerivativeforspecificyawing

7、momentGPS:GlobalPositioningSystempFuselagerollrateINS:InertialNavigationSystemqFuselagepitchrateMIMO:Multi-Input/Multi-OutputrFuselageyawrateNGC:Northrop-GrummanCorporationuControlvectoruLongitudinalv

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