无人机飞行轨迹优化外文文献翻译中英文.docx

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无人机飞行轨迹优化外文文献翻译中英文.docx

外文文献翻译

原文及译文

(本文档归max118网hh2018所有,仅供下载使用)

中文标题:

无人机的飞行路线和轨迹优化问题研究

文献出处:

期刊:

Computers&IndustrialEngineering,第120卷,

2018,页码:

116-128

译文字数:

4200多字

原文

Theunmannedaerialvehicleroutingandtrajectoryoptimisationproblem,ataxonomicreview

WaltonCoutinho,MariaBattarra,JörgFliege

Abstract:

Overthepastfewyears,UnmannedAerialVehicles(UAVs)havebecomemoreandmorepopular.ThecomplexityofroutingUAVshasnotbeenfullyinvestigatedintheliterature.Inthispaper,weprovideaformaldefinitionoftheUAVRoutingandTrajectoryOptimisationProblem(UAVRTOP).Next,weintroduceataxonomyandreviewrecentcontributionsinUAVtrajectoryoptimisation,UAVroutingandarticlesaddressingtheseproblems,andtheirvariants,simultaneously.Weconcludewiththeidentificationoffutureresearchopportunities.

Keywords:

Unmannedaerialvehicles,Routing,Trajectoryoptimization,Literaturereview,Taxonomy

Introduction

UnmannedAerialVehicles(UAVs)areaircraftthatdonotneedahumanpilotonboard.Ingeneral,thesevehiclesareeithercontrolledbyanembeddedcomputerorbyapilotoperatingaremotecontrol.Drones,remotecontrolledhelicoptersandunmannedglidersareexamplesofUAVs.Glidersdifferfromtheothertypesduetothelackofon-boardpropulsion(e.g.,anelectricorcombustionengine).ModernUAVswerefirstdevelopedinthe1920stosupportmilitaryoperationsinwhichthe

presenceofhumanpilotswaseitherimpossibleortoodangerous(BeardandMcLain,2012,KeaneandCarr,2013).However,UAVshaverecentlybecomeverypopularforlogisticsandsurveillanceapplications(Tsourdos,White,&Shanmugavel,2010).

AreportfromtheNationalPurchaseDiaryhasshownthatsalesofdronesincreasedby224%intwelvemonthsfromApril2015,reachingatotalof200 milliondollars(NPD,2016).Duetobeingabletoembedseveraltransmitters,sensorsandphotographicequipment,UAVscanbeusedinalargerangeofapplications.Successfulcaseshavebeenreportedin,forexample,aerialreconnaissance(Ruzgiené,Bertes̆ka,Gec̆yte,Jakubauskiené,&Aksamitauskas,2015),aerialforestfiredetection(Yuan,Zhang,&Liu,2015),targetobservation(Rysdyk,2006),trafficmonitoringandmanagement(Kanistras,Martins,Rutherford,&Valavanis,2013),onlinecommerce(Wang,Poikonen,&Golden,2017),geographicalmonitoring(Uysal,Toprak,&Polat,2015),scientificdatacollection(Stöcker,Eltner,&Karrasch,2015),meteorologicalsampling(Elstonetal.,2014)anddisasterassessmentandresponse(Nedjatietal.,2016,Quaritschetal.,2010,Xuetal.,2014).InHayat,Yanmaz,andMuzaffar(2016),severalapplicationsofUAVnetworksarereviewed.TheuseofUAVsfor3DmappingissurveyedinNexandRemondino(2013).AliteraturereviewabouttheapplicationsofUAVsinhumanitarianreliefisprovidedbyBravoandLeiras(2015).More

examplesofthegrowingapplicationsofUAVsarepresentedinRao,Gopi,andMaione(2016).

TheacademicroutingcommunityhasacknowledgedtheinterestofcompaniesandorganisationsinadoptingUAVsintheiroperations.ArecentexampleistheapproachofcombiningUAVsandtrucksfordistributionactivitiesbydispatchingdronesfromtrucksforthelastmiledistributionwithincitycentres(Haetal.,2015,MurrayandChu,2015,Wangetal.,2017).Ithasbeenshownthatthissolutioncanreducetrucktraveltime,andthecorrespondingCO2emissions,byupto50%.TheUAVTaskAssignmentProblem(UAVTAP),whichiscloselyrelatedtotheUAVroutingproblem,consistsofoptimisingtheassignmentofasetofUAVstoasetoftaskssubjecttomissionconstraints(Khamis,Hussein,&Elmogy,2015).AgrowingbodyofliteratureappearedontheUAVTAPinthelastdecade,e.g.,Ramirez-Atenciaetal.,inpress,Wangetal.,2015,Huetal.,2015a,Thietal.,2012,Alidaee,Gao,andWang(2010)andEdisonandShima(2011).However,theUAVroutingandtaskassignmentliteratureshaveoftenneglectedconstraintsduetotheflightdynamicsoftheUAVs.FindingfeasibletrajectoriesforUAVsinaroutingproblemisacomplextask,butitisnecessarytoensurethefeasibilityoftheUAVsroutes.Forsomereal-worldapplicationsinvolvingmorecomplexUAVsystems,suchasunmannedglidersandfixed-wingvehicles,thedefinitionofroutesmust

becoupledtothedesignofflyabletrajectories,otherwisetheassignedroutesmightbecomeinefficientoreveninfeasiblefortheseUAVs.

MostoftheUAVsusedforcivilapplicationspresentalowflightautonomy.Therefore,itisimportantforUAVroutingalgorithmstoproperlymodelbatterylife.AccordingtoFügenschuhandMüllenstedt(2015),thiscanbeachievedbyintegratingtheUAVs’dynamicswithrouting.Asmentionedbytheauthors,forpoweredUAVs,apropermodellingoftheactualfuelconsumptionmustinclude,forinstance,thecurrentweight,thealtitude,thespeedandclimb/descentrate,whichareusuallymodelledbyflightdynamics.

Zhang,Chen,andShen(2012)consideraproblemwhereaUAVmustvisitasetoftargets.However,afterreachingapredetermineddistancefromatargettheUAVmustthenadjustitsflightattitude(i.e.,itsorientation)inordertoperformapayloaddelivery.Afterthedelivery,theUAVmustcompleteanescapemanoeuvreandprepareforthenextdelivery.AccordingtoZhangetal.(2012),routingandtrajectoryoptimisationmustbeintegratedinordertoensurethesafetyofthevehicleandthefeasibilityoftrajectories.

ThecomputationoftrajectoriesforUAVshasbeenwidelystudiedintheaerospaceengineeringandoptimalcontrolliterature(Yangetal.,2016).TheTrajectoryOptimisation(TO)problemconsistsoffindingacontrolhistoryofagivenvehicle,thatminimisesascalarperformance

index(forexample,flighttimeorfuelconsumption)whilesatisfyingconstraintsonthekinematics(position,velocityandacceleration)andthedynamics(forcesandmoments)ofthevehicle(Betts,1998).AtrajectoryisgenerallyassociatedwithasetofEquationsofMotion(EOMs)thatdescribetherelationshipbetweenthespatialandthetemporalchangestothesystem.TheTOproblemiscloselyrelatedtotheOptimalControl(OC)problem(Betts,2001).

TheproblemnamedPathPlanning(PP)consistsoffindingaflyablepathforaUAVvisitingagivensequenceofwaypoints(targets)inatwo-dimensional(2D)orthree-dimensional(3D)spacewithoutconsideringthevehicle’sdynamics.AccordingtoGasparetto,Boscariol,Lanzutti,andVidoni(2015),PPisageometricproblem,becauseitisdefinedasfindingageometricpathregardlessanyspecifiedtimelaw.Inturn,TOconsistsofassigningatimelawtoacontrolledgeometricpath.

MorecomplexvariantsofthePPproblemincluding,forinstance,windandmotionconstraints,requiresubstantialsimplificationsandassumptionstobesolvedheuristically(Kunchevetal.,2006,RathinamandSengupta,2007).ThebooksbyTsourdosetal.(2010)andBeardandMcLain(2012)providegoodoverviewsofPPalgorithmsforUAVs.Ontheotherhand,highfidelityTOmodels(i.e.,usingmoreaccuratephysicalmodels)havebeendevelopedforaircraftandspacecraft(Conway,2010,Colasurdoetal.,2014,Fisch,2011,García-Herasetal.,

2014,Raivioetal.,1996).ThesemodelsarecurrentlysolvedbyOCtechniques.AnoverviewofOCmethodsforTOisprovidedinBetts,1998,Betts,2001.

ThefieldofTOhashowevernotconsideredroutingdecisions:

givenasetoforderedwaypoints,itispossibletofindafeasibletrajectoryforagenericUAV,butitisnotclearintheliteratureifthesequenceofwaypointsisappropriate.Forexample,foraglidingvehicle(i.e.,withnoonboardthrust)agivenwaypointsequencemightbeinfeasibleintermsofflightdynamics.GivenafleetofUAVs,itisanopenquestionhowtocombineroutingandtrajectorydecisionsinasingleoptimisationproblem.Asfarastheauthorsareaware,thereisnotasurveysummarisingtheliteratureaboutroutingandtrajectoryoptimisationforUAVs.

ResearchaboutintegratedroutingandTOproblemsseemstobestillfragmented.OneofthemaincontributionsofthispaperisintroducingtheUAVRoutingandTrajectoryOptimisationProblem(UAVRTOP).WebelievethatintegratingTOandroutinginasingleoptimisationproblemisakeyresearchchallengeinadoptingUAVsforrealworldapplications.

ThepurposeofthissurveyistopresenttheUAVRTOP,highlightingapproachesalreadyproposedintheliteratureandprovidingadirectionforfurtherresearch.Weintroduceataxonomy,thatisabletoidentifythekeycomponentsofroutingandTOproblems,aswellashighlightassumptionsandsimplificationscommonlyadoptedintheliterature.

Thetrajectoryoptimisationproblem

TOPsareaspecialcaseofOCproblemsdeterminingthetrajectoryofasystem(e.g.,vehiclessuchasspacecraft,aircraft,UAVs)whileminimisingameasureofperformanceandsatisfyingasetofboundary(initialandfinal)conditions,pathconstraintsandsystemdynamics.

TheoriginofOCproblemsdatestoasearlyasthe17thcenturywhenJohannBernoulliproposedtheBrachistochroneproblem(Ross,2009),oneofthefirstproblemsincalculusofvariations.OneofthefirstapplicationsofthecalculusofvariationstothecontrolofflyingvehicleswaspresentedbyRobertGoddardin“Amethodofreachingextremealtitudes”(Goddard,1919),wheretheobjectivewastodeterminetheminimuminitialmassofaground-basedrocketnecessarytoachieveagivenaltitude.OCmethodsareaclassicaltoolinthecomputationofspacecrafttrajectories,e.g.,forinterplanetarytravelandsatellitetransferorbitsaroundEarth(Conway,2010,Colasurdoetal.,2014).

Usually,systemdynamicsaremodelle

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