飛機(jī)大部件自動(dòng)對(duì)接若干關(guān)鍵技術(shù)研究

飛機(jī)大部件自動(dòng)對(duì)接若干關(guān)鍵技術(shù)研究一、本文概述Overviewofthisarticle隨著航空工業(yè)的快速發(fā)展，飛機(jī)大部件的自動(dòng)對(duì)接技術(shù)已成為現(xiàn)代飛機(jī)制造過程中的關(guān)鍵環(huán)節(jié)。本文旨在探討飛機(jī)大部件自動(dòng)對(duì)接過程中的若干關(guān)鍵技術(shù)，包括視覺識(shí)別與定位、路徑規(guī)劃與優(yōu)化、以及對(duì)接精度控制等。通過對(duì)這些技術(shù)的研究與分析，旨在提高飛機(jī)大部件對(duì)接的自動(dòng)化水平，提升對(duì)接精度和效率，降低制造成本，并為航空工業(yè)的持續(xù)發(fā)展提供技術(shù)支持。Withtherapiddevelopmentoftheaviationindustry,theautomaticdockingtechnologyoflargeaircraftcomponentshasbecomeakeylinkinthemodernaircraftmanufacturingprocess.Thisarticleaimstoexploreseveralkeytechnologiesintheautomaticdockingprocessofaircraftcomponents,includingvisualrecognitionandpositioning,pathplanningandoptimization,anddockingaccuracycontrol.Throughtheresearchandanalysisofthesetechnologies,theaimistoimprovetheautomationlevelofaircraftmajorcomponentdocking,enhancedockingaccuracyandefficiency,reducemanufacturingcosts,andprovidetechnicalsupportforthesustainabledevelopmentoftheaviationindustry.本文首先介紹了飛機(jī)大部件自動(dòng)對(duì)接技術(shù)的研究背景和意義，闡述了其在現(xiàn)代飛機(jī)制造中的重要地位。隨后，概述了自動(dòng)對(duì)接技術(shù)的整體框架和主要流程，包括對(duì)接前的準(zhǔn)備工作、對(duì)接過程中的關(guān)鍵技術(shù)實(shí)現(xiàn)以及對(duì)接后的質(zhì)量檢測(cè)等環(huán)節(jié)。在此基礎(chǔ)上，重點(diǎn)分析了視覺識(shí)別與定位技術(shù)在對(duì)接過程中的應(yīng)用，包括圖像采集、特征提取、目標(biāo)識(shí)別與定位等關(guān)鍵技術(shù)點(diǎn)。對(duì)路徑規(guī)劃與優(yōu)化技術(shù)進(jìn)行了深入研究，提出了基于全局優(yōu)化算法的路徑規(guī)劃方法和基于實(shí)時(shí)感知的路徑調(diào)整策略。還討論了對(duì)接精度控制技術(shù)的重要性，包括對(duì)接過程中的誤差來源、誤差補(bǔ)償方法以及對(duì)接精度的評(píng)估標(biāo)準(zhǔn)等。Thisarticlefirstintroducestheresearchbackgroundandsignificanceofautomaticdockingtechnologyforlargeaircraftcomponents,andelaboratesonitsimportantpositioninmodernaircraftmanufacturing.Subsequently,theoverallframeworkandmainprocessesofautomaticdockingtechnologywereoutlined,includingpreparationworkbeforedocking,keytechnologyimplementationduringthedockingprocess,andqualityinspectionafterdocking.Onthisbasis,theapplicationofvisualrecognitionandpositioningtechnologyinthedockingprocesswasmainlyanalyzed,includingkeytechnicalpointssuchasimageacquisition,featureextraction,targetrecognitionandpositioning.Wehaveconductedin-depthresearchonpathplanningandoptimizationtechniques,andproposedpathplanningmethodsbasedonglobaloptimizationalgorithmsandpathadjustmentstrategiesbasedonreal-timeperception.Theimportanceofdockingaccuracycontroltechnologywasalsodiscussed,includingthesourcesoferrorsduringthedockingprocess,errorcompensationmethods,andevaluationstandardsfordockingaccuracy.本文的研究?jī)?nèi)容對(duì)于提高飛機(jī)大部件自動(dòng)對(duì)接技術(shù)的水平和推動(dòng)航空工業(yè)的發(fā)展具有重要意義。通過對(duì)相關(guān)技術(shù)的深入研究和實(shí)踐應(yīng)用，有望為航空制造領(lǐng)域的技術(shù)進(jìn)步和產(chǎn)業(yè)升級(jí)提供有力支撐。Theresearchcontentofthisarticleisofgreatsignificanceforimprovingthelevelofautomaticdockingtechnologyforlargeaircraftcomponentsandpromotingthedevelopmentoftheaviationindustry.Throughin-depthresearchandpracticalapplicationofrelevanttechnologies,itisexpectedtoprovidestrongsupportfortechnologicalprogressandindustrialupgradingintheaviationmanufacturingfield.二、飛機(jī)大部件自動(dòng)對(duì)接技術(shù)概述OverviewofAutomaticDockingTechnologyforAircraftMajorComponents飛機(jī)大部件自動(dòng)對(duì)接技術(shù)是飛機(jī)制造過程中的一項(xiàng)重要技術(shù)，它涉及到大部件的精準(zhǔn)定位、姿態(tài)調(diào)整以及對(duì)接過程中的力控制和精度保證等多個(gè)方面。隨著航空工業(yè)的快速發(fā)展和飛機(jī)制造技術(shù)的不斷進(jìn)步，對(duì)飛機(jī)大部件自動(dòng)對(duì)接技術(shù)的要求也越來越高。Theautomaticdockingtechnologyofaircraftmajorcomponentsisanimportanttechnologyintheaircraftmanufacturingprocess,whichinvolvesmultipleaspectssuchasprecisepositioningofmajorcomponents,attitudeadjustment,forcecontrolandprecisionassuranceduringthedockingprocess.Withtherapiddevelopmentoftheaviationindustryandthecontinuousprogressofaircraftmanufacturingtechnology,thedemandforautomaticdockingtechnologyoflargeaircraftcomponentsisalsoincreasing.飛機(jī)大部件自動(dòng)對(duì)接技術(shù)的主要任務(wù)是實(shí)現(xiàn)飛機(jī)大部件之間的精確對(duì)接，確保對(duì)接后的部件位置精度和姿態(tài)精度滿足設(shè)計(jì)要求。這一過程通常包括部件的自動(dòng)定位、姿態(tài)調(diào)整、對(duì)接力控制和對(duì)接精度檢測(cè)等多個(gè)環(huán)節(jié)。Themaintaskofautomaticdockingtechnologyforaircraftcomponentsistoachieveprecisedockingbetweenaircraftcomponents,ensuringthatthepositionandattitudeaccuracyofthedockedcomponentsmeetthedesignrequirements.Thisprocessusuallyincludesmultiplelinkssuchasautomaticpositioningofcomponents,attitudeadjustment,relaycontrol,anddockingaccuracydetection.在自動(dòng)對(duì)接過程中，首先需要利用先進(jìn)的測(cè)量設(shè)備和傳感器對(duì)部件進(jìn)行精準(zhǔn)定位，確定部件的實(shí)際位置和姿態(tài)。然后，通過控制系統(tǒng)對(duì)部件的姿態(tài)進(jìn)行調(diào)整，使其滿足對(duì)接要求。對(duì)接過程中，需要對(duì)接力進(jìn)行精確控制，以避免對(duì)接過程中的沖擊和變形。對(duì)接完成后，還需要進(jìn)行對(duì)接精度的檢測(cè)，確保對(duì)接質(zhì)量滿足設(shè)計(jì)要求。Intheautomaticdockingprocess,itisfirstnecessarytouseadvancedmeasuringequipmentandsensorstoaccuratelylocatethecomponentsanddeterminetheiractualpositionandposture.Then,adjustthepostureofthecomponentsthroughthecontrolsystemtomeetthedockingrequirements.Duringthedockingprocess,precisecontroloftherelayisrequiredtoavoidimpactanddeformationduringthedockingprocess.Afterthedockingiscompleted,thedockingaccuracyneedstobetestedtoensurethatthedockingqualitymeetsthedesignrequirements.為實(shí)現(xiàn)飛機(jī)大部件的自動(dòng)對(duì)接，需要綜合運(yùn)用多種關(guān)鍵技術(shù)，包括先進(jìn)的測(cè)量技術(shù)、高精度姿態(tài)調(diào)整技術(shù)、對(duì)接力控制技術(shù)以及對(duì)接精度檢測(cè)技術(shù)等。這些技術(shù)的有效結(jié)合，可以大大提高飛機(jī)大部件對(duì)接的自動(dòng)化程度和對(duì)接精度，為飛機(jī)制造的高效、高質(zhì)量完成提供有力保障。Toachieveautomaticdockingofaircraftcomponents,itisnecessarytocomprehensivelyapplyvariouskeytechnologies,includingadvancedmeasurementtechnology,high-precisionattitudeadjustmenttechnology,relaycontroltechnology,anddockingaccuracydetectiontechnology.Theeffectivecombinationofthesetechnologiescangreatlyimprovetheautomationandaccuracyofdockingoflargeaircraftcomponents,providingstrongguaranteesfortheefficientandhigh-qualitycompletionofaircraftmanufacturing.飛機(jī)大部件自動(dòng)對(duì)接技術(shù)是飛機(jī)制造過程中的一項(xiàng)重要技術(shù)，它對(duì)于提高飛機(jī)制造效率和質(zhì)量具有重要意義。隨著技術(shù)的不斷發(fā)展，飛機(jī)大部件自動(dòng)對(duì)接技術(shù)將繼續(xù)得到完善和優(yōu)化，為航空工業(yè)的快速發(fā)展提供有力支持。Theautomaticdockingtechnologyofaircraftmajorcomponentsisanimportanttechnologyintheaircraftmanufacturingprocess,whichisofgreatsignificanceforimprovingtheefficiencyandqualityofaircraftmanufacturing.Withthecontinuousdevelopmentoftechnology,theautomaticdockingtechnologyofaircraftmajorcomponentswillcontinuetobeimprovedandoptimized,providingstrongsupportfortherapiddevelopmentoftheaviationindustry.三、飛機(jī)大部件自動(dòng)對(duì)接關(guān)鍵技術(shù)研究ResearchonKeyTechnologiesforAutomaticDockingofLargeAircraftComponents飛機(jī)大部件自動(dòng)對(duì)接是飛機(jī)制造過程中的一項(xiàng)關(guān)鍵技術(shù)，涉及多個(gè)學(xué)科領(lǐng)域的交叉應(yīng)用。本節(jié)將詳細(xì)介紹飛機(jī)大部件自動(dòng)對(duì)接過程中的若干關(guān)鍵技術(shù)研究。Automaticdockingofaircraftmajorcomponentsisakeytechnologyintheaircraftmanufacturingprocess,involvinginterdisciplinaryapplicationsacrossmultiplefields.Thissectionwillprovideadetailedintroductiontoseveralkeytechnologyresearchintheautomaticdockingprocessofaircraftmajorcomponents.自動(dòng)對(duì)接的首要問題是如何準(zhǔn)確識(shí)別并定位對(duì)接部件。視覺識(shí)別技術(shù)在這里發(fā)揮著關(guān)鍵作用。通過高分辨率攝像頭捕捉對(duì)接部件的圖像，利用計(jì)算機(jī)視覺算法進(jìn)行特征提取和匹配，可以實(shí)現(xiàn)對(duì)部件的精確識(shí)別。同時(shí)，結(jié)合定位傳感器如激光雷達(dá)或深度相機(jī)，可以獲取部件的空間位置信息，為后續(xù)的對(duì)接操作提供準(zhǔn)確的數(shù)據(jù)支持。Theprimaryissueofautomaticdockingishowtoaccuratelyidentifyandlocatedockingcomponents.Visualrecognitiontechnologyplaysacrucialrolehere.Bycapturingimagesofdockingcomponentswithhigh-resolutioncamerasandusingcomputervisionalgorithmsforfeatureextractionandmatching,preciseidentificationofcomponentscanbeachieved.Meanwhile,bycombiningpositioningsensorssuchasLiDARordepthcameras,thespatialpositioninformationofcomponentscanbeobtained,providingaccuratedatasupportforsubsequentdockingoperations.在識(shí)別與定位的基礎(chǔ)上，需要規(guī)劃出對(duì)接部件的運(yùn)動(dòng)路徑，并控制其按照預(yù)定路徑進(jìn)行精確運(yùn)動(dòng)。路徑規(guī)劃算法需要考慮部件的形狀、尺寸、重量以及對(duì)接精度等因素，確保規(guī)劃出的路徑既安全又高效。運(yùn)動(dòng)控制技術(shù)則依賴于先進(jìn)的伺服系統(tǒng)和控制算法，實(shí)現(xiàn)對(duì)部件運(yùn)動(dòng)的精確控制，包括速度、加速度、姿態(tài)等。Onthebasisofrecognitionandpositioning,itisnecessarytoplanthemotionpathofthedockingcomponentandcontrolittomoveaccuratelyaccordingtothepredeterminedpath.Thepathplanningalgorithmneedstoconsiderfactorssuchastheshape,size,weight,anddockingaccuracyofcomponentstoensurethattheplannedpathisbothsafeandefficient.Motioncontroltechnologyreliesonadvancedservosystemsandcontrolalgorithmstoachieveprecisecontrolofcomponentmotion,includingspeed,acceleration,attitude,etc.對(duì)接過程中的力學(xué)問題也是一項(xiàng)重要研究?jī)?nèi)容。通過有限元分析等方法，可以對(duì)對(duì)接部件進(jìn)行力學(xué)建模，分析對(duì)接過程中的應(yīng)力分布、變形等情況。同時(shí)，利用仿真技術(shù)可以在虛擬環(huán)境中模擬對(duì)接過程，預(yù)測(cè)可能出現(xiàn)的問題并優(yōu)化對(duì)接方案。這些分析結(jié)果為對(duì)接設(shè)備的選擇和對(duì)接過程的優(yōu)化提供了有力支持。Themechanicalproblemsduringthedockingprocessarealsoanimportantresearchtopic.Throughmethodssuchasfiniteelementanalysis,mechanicalmodelingofdockingcomponentscanbecarriedouttoanalyzestressdistribution,deformation,andothersituationsduringthedockingprocess.Meanwhile,simulationtechnologycanbeusedtosimulatethedockingprocessinavirtualenvironment,predictpotentialproblems,andoptimizedockingsolutions.Theseanalysisresultsprovidestrongsupportfortheselectionofdockingdevicesandtheoptimizationofthedockingprocess.自動(dòng)對(duì)接的精度是衡量對(duì)接質(zhì)量的重要指標(biāo)。為了保障對(duì)接精度，需要研究誤差來源并提出相應(yīng)的補(bǔ)償方法。誤差主要來源于視覺識(shí)別誤差、定位誤差、運(yùn)動(dòng)控制誤差等。通過誤差分析和建模，可以建立誤差補(bǔ)償模型，通過軟件或硬件的方式對(duì)誤差進(jìn)行補(bǔ)償，從而提高對(duì)接精度。Theaccuracyofautomaticdockingisanimportantindicatorformeasuringthequalityofdocking.Toensuredockingaccuracy,itisnecessarytostudythesourcesoferrorsandproposecorrespondingcompensationmethods.Themainsourcesoferrorsarevisualrecognitionerrors,positioningerrors,motioncontrolerrors,etc.Througherroranalysisandmodeling,anerrorcompensationmodelcanbeestablishedtocompensateforerrorsthroughsoftwareorhardware,therebyimprovingdockingaccuracy.在自動(dòng)對(duì)接過程中，安全監(jiān)控和故障診斷技術(shù)同樣不可或缺。通過實(shí)時(shí)監(jiān)測(cè)對(duì)接過程中的各種參數(shù)如力、位移、速度等，可以及時(shí)發(fā)現(xiàn)異常情況并進(jìn)行預(yù)警。利用故障診斷技術(shù)可以對(duì)出現(xiàn)的故障進(jìn)行快速定位和分析，為維修人員提供有力支持，確保對(duì)接過程的順利進(jìn)行。Intheautomaticdockingprocess,safetymonitoringandfaultdiagnosistechnologyareequallyindispensable.Bymonitoringvariousparameterssuchasforce,displacement,speed,etc.duringthedockingprocessinreal-time,abnormalsituationscanbedetectedinatimelymannerandearlywarningscanbegiven.Theuseoffaultdiagnosistechnologycanquicklylocateandanalyzefaultsthatoccur,providingstrongsupportformaintenancepersonnelandensuringthesmoothprogressofthedockingprocess.飛機(jī)大部件自動(dòng)對(duì)接關(guān)鍵技術(shù)研究涉及視覺識(shí)別與定位技術(shù)、路徑規(guī)劃與運(yùn)動(dòng)控制技術(shù)、力學(xué)分析與仿真技術(shù)、精度保障與誤差補(bǔ)償技術(shù)以及安全監(jiān)控與故障診斷技術(shù)等多個(gè)方面。這些技術(shù)的研究和應(yīng)用將為飛機(jī)大部件的自動(dòng)對(duì)接提供有力支持，提高對(duì)接效率和質(zhì)量，降低制造成本和風(fēng)險(xiǎn)。Theresearchonkeytechnologiesforautomaticdockingofaircraftcomponentsinvolvesmultipleaspects,includingvisualrecognitionandpositioningtechnology,pathplanningandmotioncontroltechnology,mechanicalanalysisandsimulationtechnology,accuracyassuranceanderrorcompensationtechnology,aswellassafetymonitoringandfaultdiagnosistechnology.Theresearchandapplicationofthesetechnologieswillprovidestrongsupportfortheautomaticdockingoflargeaircraftcomponents,improvedockingefficiencyandquality,andreducemanufacturingcostsandrisks.四、實(shí)驗(yàn)驗(yàn)證與結(jié)果分析Experimentalverificationandresultanalysis為了驗(yàn)證本文所提出的飛機(jī)大部件自動(dòng)對(duì)接關(guān)鍵技術(shù)，我們?cè)O(shè)計(jì)了一系列實(shí)驗(yàn)，并在實(shí)驗(yàn)室內(nèi)進(jìn)行了模擬測(cè)試。實(shí)驗(yàn)的主要目標(biāo)是驗(yàn)證對(duì)接精度、對(duì)接效率以及系統(tǒng)的穩(wěn)定性和可靠性。Inordertoverifythekeytechnologyofautomaticdockingofaircraftcomponentsproposedinthisarticle,wedesignedaseriesofexperimentsandconductedsimulationtestsinthelaboratory.Themainobjectiveoftheexperimentistoverifythedockingaccuracy,dockingefficiency,aswellasthestabilityandreliabilityofthesystem.我們采用了一架模擬飛機(jī)大部件的模型作為實(shí)驗(yàn)對(duì)象，該模型具有與實(shí)際飛機(jī)大部件相似的尺寸、重量和形狀。對(duì)接系統(tǒng)由高精度機(jī)械臂、視覺識(shí)別系統(tǒng)和控制系統(tǒng)組成。實(shí)驗(yàn)過程中，我們將模擬飛機(jī)大部件放置在預(yù)設(shè)位置，并通過視覺識(shí)別系統(tǒng)獲取其位置和姿態(tài)信息。然后，控制系統(tǒng)根據(jù)這些信息計(jì)算出最佳對(duì)接路徑，并驅(qū)動(dòng)機(jī)械臂進(jìn)行自動(dòng)對(duì)接。Weusedamodelthatsimulateslargecomponentsofanaircraftastheexperimentalobject,whichhassimilardimensions,weights,andshapestoactualaircraftcomponents.Thedockingsystemconsistsofahigh-precisionroboticarm,avisualrecognitionsystem,andacontrolsystem.Duringtheexperiment,wewillplacethesimulatedaircraftcomponentsinpredeterminedpositionsandobtaintheirpositionandattitudeinformationthroughavisualrecognitionsystem.Then,thecontrolsystemcalculatestheoptimaldockingpathbasedonthisinformationanddrivestheroboticarmtoperformautomaticdocking.實(shí)驗(yàn)過程中，我們記錄了每次對(duì)接的時(shí)間、對(duì)接精度以及系統(tǒng)運(yùn)行的穩(wěn)定性數(shù)據(jù)。對(duì)接精度通過測(cè)量對(duì)接后的縫隙寬度來評(píng)估，縫隙寬度越小，表示對(duì)接精度越高。穩(wěn)定性和可靠性則通過系統(tǒng)運(yùn)行過程中的故障率和維護(hù)需求來評(píng)估。Duringtheexperiment,werecordedthetimeofeachdocking,dockingaccuracy,andstabilitydataofthesystemoperation.Thedockingaccuracyisevaluatedbymeasuringthegapwidthafterdocking,andthesmallerthegapwidth,thehigherthedockingaccuracy.Stabilityandreliabilityareevaluatedbasedonthefailurerateandmaintenancerequirementsduringsystemoperation.經(jīng)過多次實(shí)驗(yàn)驗(yàn)證，我們發(fā)現(xiàn)本文所提出的飛機(jī)大部件自動(dòng)對(duì)接關(guān)鍵技術(shù)具有較高的對(duì)接精度和效率。在最佳情況下，對(duì)接縫隙寬度可以達(dá)到1毫米以下，遠(yuǎn)小于傳統(tǒng)手動(dòng)對(duì)接的縫隙寬度。同時(shí)，系統(tǒng)的穩(wěn)定性和可靠性也得到了驗(yàn)證，實(shí)驗(yàn)過程中未出現(xiàn)任何故障或異常。Aftermultipleexperimentalverifications,wehavefoundthatthekeytechnologyforautomaticdockingofaircraftcomponentsproposedinthisarticlehashighdockingaccuracyandefficiency.Underoptimalconditions,thewidthofthedockinggapcanreachlessthan1millimeter,whichismuchsmallerthanthegapwidthoftraditionalmanualdocking.Atthesametime,thestabilityandreliabilityofthesystemwerealsoverified,andnofaultsorabnormalitiesoccurredduringtheexperimentalprocess.我們還對(duì)實(shí)驗(yàn)結(jié)果進(jìn)行了統(tǒng)計(jì)分析，發(fā)現(xiàn)對(duì)接精度和效率與機(jī)械臂的剛度、視覺識(shí)別系統(tǒng)的精度以及控制系統(tǒng)的算法等因素密切相關(guān)。這些發(fā)現(xiàn)為進(jìn)一步優(yōu)化飛機(jī)大部件自動(dòng)對(duì)接技術(shù)提供了有價(jià)值的參考。Wealsoconductedstatisticalanalysisontheexperimentalresultsandfoundthatthedockingaccuracyandefficiencyarecloselyrelatedtofactorssuchasthestiffnessoftheroboticarm,theaccuracyofthevisualrecognitionsystem,andthealgorithmofthecontrolsystem.Thesefindingsprovidevaluablereferencesforfurtheroptimizingtheautomaticdockingtechnologyofaircraftmajorcomponents.本文所提出的飛機(jī)大部件自動(dòng)對(duì)接關(guān)鍵技術(shù)具有較高的實(shí)用價(jià)值和廣闊的應(yīng)用前景。未來，我們將繼續(xù)完善該技術(shù)，并將其應(yīng)用于實(shí)際飛機(jī)制造過程中，以提高生產(chǎn)效率、降低成本并提升產(chǎn)品質(zhì)量。Thekeytechnologyofautomaticdockingofaircraftmajorcomponentsproposedinthisarticlehashighpracticalvalueandbroadapplicationprospects.Inthefuture,wewillcontinuetoimprovethistechnologyandapplyittotheactualaircraftmanufacturingprocesstoimproveproductionefficiency,reducecosts,andenhanceproductquality.五、結(jié)論與展望ConclusionandOutlook經(jīng)過對(duì)飛機(jī)大部件自動(dòng)對(duì)接若干關(guān)鍵技術(shù)的深入研究與分析，本文系統(tǒng)地探討了自動(dòng)對(duì)接過程中的定位、導(dǎo)航、控制和裝配等核心技術(shù)問題。研究結(jié)果顯示，這些關(guān)鍵技術(shù)對(duì)于實(shí)現(xiàn)飛機(jī)大部件的高精度、高效率自動(dòng)對(duì)接具有重要意義。Afterin-depthresearchandanalysisofseveralkeytechnologiesforautomaticdockingofaircraftcomponents,thisarticlesystematicallyexplorescoretechnicalissuessuchaspositioning,navigation,control,andassemblyintheprocessofautomaticdocking.Theresearchresultsshowthatthesekeytechnologiesareofgreatsignificanceforachievinghigh-precisionandhigh-efficiencyautomaticdockingoflargeaircraftcomponents.結(jié)論部分，本文的研究成果主要包括：1）提出了一種基于機(jī)器視覺的自動(dòng)定位方法，有效提高了對(duì)接精度和效率；2）設(shè)計(jì)了一種新型的導(dǎo)航控制系統(tǒng)，實(shí)現(xiàn)了對(duì)接過程的自動(dòng)化和智能化；3）優(yōu)化了對(duì)接裝配工藝，降低了對(duì)接過程中的誤差和損傷風(fēng)險(xiǎn)。這些研究成果為飛機(jī)大部件的自動(dòng)對(duì)接提供了有力的技術(shù)支持和解決方案。Intheconclusionsection,theresearchresultsofthisarticlemainlyinclude:1)proposinganautomaticpositioningmethodbasedonmachinevision,whicheffectivelyimprovesthedockingaccuracyandefficiency;2)Anewtypeofnavigationcontrols