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簡(jiǎn)介:電子科技大學(xué)爾I呢尺8102201010801202入凡01200000八博士學(xué)位論文001010188X110電子科技大學(xué)圖標(biāo)〕論文題目航空發(fā)動(dòng)機(jī)輪盤低周疲勞壽命預(yù)測(cè)方法研究指導(dǎo)教師黃洪鐘教授686300010界0166101100610010060601060180入00010018861311008此爪111⑷10016811016010010801600630過(guò)6000100103016030103101066101111101IV71130八34801『0炙0030000700801001800010丨6031001080106610
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簡(jiǎn)介:密級(jí)公開(kāi)分類號(hào)V2322碩士學(xué)位論文作者作者指導(dǎo)教師指導(dǎo)教師丁鋒教授申請(qǐng)學(xué)位學(xué)科申請(qǐng)學(xué)位學(xué)科2017年04月18日XI’ANTECHNOLOGICALUNIVERSITY題目航空發(fā)動(dòng)機(jī)軸承可靠性及動(dòng)剛度分析機(jī)械設(shè)計(jì)及理論燕紫薇燕紫薇
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簡(jiǎn)介:工學(xué)博士學(xué)位論文非線性濾波理論在航天器姿態(tài)確定中的應(yīng)用黃琳哈爾濱工業(yè)大學(xué)2007年10月CLASSIFIEDINDEXV448224UDC629783DISSERTATIONFORTHEDOCTORALDEGREEINENGINEERINGAPPLICATIONSOFNONLINEARBAYESIANFILTERINGALGORITHMSTOSPACECRAFTATTITUDEDETERMINATIONCANDIDATEHUANGLINSUPERVISORPROFJINGWUXINGACADEMICDEGREEAPPLIEDFORDOCTOROFENGINEERINGSPECIALTYSPACECRAFTDESIGNAFFILIATIONDEPTOFASTRONAUTICENGINEERINGDATEOFDEFENCEOCTOBER,2007DEGREECONFERRINGINSTITUTIONHARBININSTITUTEOFTECHNOLOGY
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簡(jiǎn)介:南京理工大學(xué)碩士學(xué)位論文航空發(fā)動(dòng)機(jī)機(jī)匣的包容性數(shù)值分析與實(shí)驗(yàn)研究姓名李海波申請(qǐng)學(xué)位級(jí)別碩士專業(yè)工程力學(xué)指導(dǎo)教師章定國(guó)20100601ABSTRACTWHENWOR“NG’THEROTORINAIRGASTURBINEENGINEISROTATINGATAHI曲SPEEDWHENABLADEFAILUREMLADESOFTHEROTORARETOMAPARTACCIDENTALLYOCCURS,KINETICENERGYOFTHEPROJECTILESISENORMOUSBECAUSEOFCENTRIFUGALFORCEALTHOUGHTHENON。CONTAINMENTINCIDENTSELDOMOCCURS,ONCEITHAPPENSITWILLLEADTOSERIOUSAVIATIONACCIDENTACCORDINGLY,ADOPTINGFEASIBLEDESIGNAPPROACHESTOACCOMMODATELI曲。ENERGYBLADESISNECESSITATEDTHISPAPERSYSTEMATICALLYSTUDIESSEVERALISSHESCONCERNINGAERO。ENGINECASINGCONTAINNLENT,ANDVERIFIESTHEVALIDITYOFNUMERICALANALYSISBYCONDUCTINGSHOOTINGEXPERIMEMSINADDITION,ANUMERICALSIMULATIONOFACASINGOFCERTAINMODELENGINEASWELLASANEWCASINGISCARRIEDOUTTHISPAPERMAINLYFOCUSESONTHEFOLLOWINGASPECTS1CONDUCTINGSHOOTINGEXPERIMENTSANDNUMERICALSIMULATIONRELATED9SHOOTINGEXPERIMENTSARECARRIEDOUTBYCONSIDERINGDIFFERENTSPEEDSANDDIFFERENTPOSTURESOFATARGET,INDICATINGTHENUMERICALSIMULATIONAPPLIEDINTHISDOMAINISFEASIBLE2THENUMERICALANALYSISOFENGINECASINGCONTAINMENTCONTAINMENTPERFORMANCEOFCERTAINENGINEDESIGNEDINCHINAISNUMERICALLYANALYZEDFROMALLPERSPECTIVESCONTAINMENTCAPABILITYOF1ST,2NDAND3RDGRADESISANALYZEDINITIALLYTHEINTERFERENCESOFTHEFRACTUREANDBLADESREMAINED,ALONGWITHTHEIMPACTONCONTAI衄ENTINABLADEFAILUREARESTUDIEDTHECASINGCONTAINMENTOFAPRACTICALENGINELSTHEREBYEVALUATED3NUMERICALSIMULATIONOFCASINGCONTAINMENTN啪ERICALSIMULATIONSFORDOUBLEDECKENGINECASINGWITHTITANIUMALLOYINNERDECKANDCOMPOSITEOUTERDECKARECONDUCTEDTHICKNESSOFCONTAINMENTISOBTAINEDBYCHANGINGTHETLLICLMESSOFBOTHINNERANDTHEOUTERDECKTHEIMPACTONCONTAINMENTOFTHEDOUBLEDECKENGINECASINGISANALYZEDANDCOMPAREDOPTIMIZEDCLEARANCEDISTANCEWHICHPROVIDESAREFERENCEFORDEVELOPINGSLOPEENGINECASINGISDERIVEDIMPROVEMENTSOFCONTAINMENTBYADDINGFLANGESTOANENGINECASTINGAREDISCUSSEDBYCONDUCTINGNUMERICALSIMULATIONSBESIDES,THEOPTIMALQUANTITYANDLOCATIONOFFLANGESAREOBTAINEDTOINCREASECONTAINMENTTHECONTAIMNENTOFMETALCASINGWITHKEVLARAROUNDTHEOUTSIDEISANALYZED,WHICHPROVIDESAREFERENCEFORFUTUREDESIGNKEYWORDSTHEAEROENGINE,CASING,CONTAINMENT,NUMERICALSIMULATION
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簡(jiǎn)介:大連理工大學(xué)碩士學(xué)位論文兩種典型航空材料數(shù)控銑削工藝研究與優(yōu)化姓名王志鑫申請(qǐng)學(xué)位級(jí)別碩士專業(yè)機(jī)械電子工程指導(dǎo)教師金洙吉20051201王志鑫兩種媳型航空材料數(shù)控銑削工藝研究與優(yōu)化RESEARCHANDOPTIMIZATIONONNCMILLINGTECHNOLOGYFORTWOTYPICALAERONAUTICALMATERIALSABSTRACTAERONAUTICALINDUSTRIESMANUFACLUFECOMPONENTSWHHFITAAIUMALLOYS。ALUMINUMALLOYSANDALSOSPECIALSTAINLESSSTEELSTHESEINDUSTRIESARECHARACTERIZEDBYAGREATCOSTINTHEPRODUCTIONOFTHESEWORKPIECESANDO羲EOFTHEGREATREASOLLSOFTHISELEVATEDCOSTISTHETOWLEVELMACHININGEFFICIENCYFORTHISREASON,ITISINTERESTINGTOREDUCETHETIMESOFWORKPIECESMACHININGANDTOINHEREMACHININGEFFICIENCYACCORDINGTOTHESTATUSOFAERONAUTICALINDUSTRIESINOURCOUNTRY,SELECTINGTHEMACHININGCONDITIONSANDPARAMETERSISCRUCIALTHEREFORE,ALLOPTIMALSELECTIONOFCUTTINGPARAMETERSTOSATISFYANECONOMICOBJECTIVEISAVERYIMPORTANTTASKINTHEMANUFACTURINGPROCESSOFAERONAUTICALACCESSORIES,EACHMATERIALWILTSHOWITSDIFFERENTMACHININGCHARACTERISTICFOREXAMPLE,THELOWSTRENGTHOFALUMINUMALLOYSRESULTINSERIOUSMACHININGDISTORTION;THEHISTRENGTHANDLOWTHERMALCONDUCTIVITYOFTITANIUMALLOYSRESULTINSERIOUSTOOLWEARSOTHISPAPERWILLADOPTDIFFERENTMETHODSTOOPTIMIZECUTTINGPARAMETERSTOREDUCETHEMACHININGDISTORTIONANDMANUFACTURINGCOST,INEASETHEMACHININGEFFICIENCYINTHISPAPER,FIRSTLYEXPERIMENTSAREUSEDTOCONSTRUCTTHERELATIONSHIPSBETWEENTHECUTTINGFORCEANDCUTTINGPARAMETERSTOTITANIUMALLOYSANDALUMINUMALLOYSTHENBECAUSEOFTHEIRDIFFERENTMATERIALCHARACTERISTICS,SOTOALUMINMNALLOYS,SOMERESE骶CHESAREDONE韜FINDTHERULEOFTHESMNCEROUGHNESSOFTHINWEBANDTHINWALLWITHTHECUTTINGPARAMETERS;TOTITANIUMALLOYS,THEMECHANISMOFTOOLWEAL“ISRESEARCHEDFINALLY,TOALUMINUMALLOYSMACHIHING,THEOPTIMALRANGEOFCUTTINGPARAMETERSWASPRESENTEDTOTITANIUMALLOYSMACHINING,ALLOPTIMIZATIONALGORITHMWHICHISCALLEDIDEALPOINTMETHODISTHENAPPLIEDTOTHEMODELFORDETERMININGOPTIMALCUTTINGPARAMETERS。THEOPTIMALCUTTINGPARAMETERSARESUBJECT蕊TOTWOOBJECTIVEFUNCTIONSOFMAXIMUMPRODUCTIONRATEANDMINIMUMPRODUCTIONCOSTWITLLTHECONSTRAINTSOFCUTTINGFORCEANDTHEUSERSCALLSELECTAPPROPRIATEPARAMETERSBASEONPRACTICALNEED。KEYWORDSAERONAUTICALMATERIAL;ALUMINUMALLOY;TITANIUMALLOY;MILLING;OPTIMIZATION。II。
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簡(jiǎn)介:分類號(hào)0351密級(jí)洳;≥.唼博士學(xué)位論文單位代碼學(xué)號(hào)1033511224009中文論文題目塹窒搓迪旦翌二蕉監(jiān)墨匡杰澧速籃熱盤裂鯉夔墊丑塞數(shù)熬焦蕉擬翌窺英文論文題目NUMERICALSTUDIESOFTURBULENTHEATTRANSFERANDENDOTHERMICPYROLYSISOFAVIATIONKEROSENERP3型§女旦絲西±I£41P£5§盟§申請(qǐng)人姓名筮衛(wèi)亙指導(dǎo)教師垂垡塑撞臺(tái)作導(dǎo)師專業(yè)名稱蘊(yùn)佳直堂研究方向超蝤晝匡左佳墊所在學(xué)院藍(lán)窒航丞堂醫(yī)論文提交日期201746AUTH。R,SS;GNATU瞅睦K2叢SUPERVISOR’SSIGNATUREEXTEMALREVIEWERSEXAMININGCOMMITTEECHAIRPERSON.WEIFANGCHENKPROFESSOR\ZHEIIANGUNIVERSITY....一EXAMININGCOMMITTEEMEMBERS魚(yú)QQ邁里£Q魚(yú)墨墨Q亟自I塑G墮遜Y星墨I(xiàn)鯉WENJUNFANGKPROFESSORUZHEJIANGUNIVERSITY............£H塹G墨H金墜G圣H墜選QI壘曼壘Q£堅(jiān)H自I墾墜G墮壘疊叢I£墨煎YEL墜墾墜壘曼壘G塑QL壘墨墨Q£豎H自I壘塾G墮墜IY曼£曼塹AL一DATEOFORALDEFENCE叢型壘,2QZ
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簡(jiǎn)介:中國(guó)科學(xué)技術(shù)大學(xué)博士學(xué)位論文基于證據(jù)理論的在軌航天器故障診斷方法研究姓名梁偉光申請(qǐng)學(xué)位級(jí)別博士專業(yè)導(dǎo)航、制導(dǎo)與控制指導(dǎo)教師王永周建亮201105摘要II驗(yàn)進(jìn)行驗(yàn)證。本文第五章選用了協(xié)同工作類故障和振動(dòng)發(fā)散類故障兩類有代表性故障進(jìn)行實(shí)驗(yàn)研究。其中,協(xié)同工作類故障的實(shí)驗(yàn)數(shù)據(jù)采用航天實(shí)測(cè)數(shù)據(jù),振動(dòng)發(fā)散類故障的數(shù)據(jù)選用具有代表性的隔振系統(tǒng)振動(dòng)發(fā)散類故障數(shù)據(jù)。分別從故障表現(xiàn)、證據(jù)生成、融合診斷等方面對(duì)診斷過(guò)程加以實(shí)現(xiàn),并根據(jù)振動(dòng)發(fā)散類故障診斷過(guò)程中出現(xiàn)的傳感器數(shù)據(jù)傳輸出錯(cuò)的問(wèn)題進(jìn)行了容錯(cuò)性改進(jìn),設(shè)計(jì)了證據(jù)重構(gòu)方法。未備案故障的診斷具有重要意義,但利用現(xiàn)有的證據(jù)理論融合診斷框架無(wú)法實(shí)現(xiàn)對(duì)未備案故障的診斷。本文第六章對(duì)利用證據(jù)理論診斷未備案故障的問(wèn)題進(jìn)行了探索性研究。首先分析了未備案故障的證據(jù)表現(xiàn)形式,進(jìn)而選取開(kāi)放世界思想和證據(jù)折扣方法形成了融合診斷機(jī)理。分別考慮故障焦元無(wú)交集和有傳遞性交集的兩種情況,對(duì)開(kāi)放框架下的折扣融合過(guò)程進(jìn)行理論推導(dǎo),并設(shè)計(jì)仿真實(shí)驗(yàn)驗(yàn)證了方法在診斷未備案故障方面的有效性與合理性。關(guān)鍵詞關(guān)鍵詞證據(jù)理論故障診斷信息融合在軌航天器信息熵診斷窗口協(xié)同工作振動(dòng)發(fā)散未備案故障開(kāi)放診斷框架證據(jù)折扣
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簡(jiǎn)介:分類號(hào)UDC一密級(jí)學(xué)號(hào)公玨028030609中國(guó)民用航空學(xué)院碩士學(xué)位論文航空發(fā)動(dòng)機(jī)零部件的試驗(yàn)?zāi)B(tài)分析及應(yīng)用研究生姓名儉二鳴導(dǎo)師姓名奎主墮數(shù)援申請(qǐng)學(xué)位級(jí)別亟學(xué)科專業(yè)名稱藍(lán)窒主魅撞進(jìn)堡迨與王猩所在院系扭皇堂瞳論文答辯日期2QQ圭旦2旦2005年1月15日塑墾里墮窒堂墮堡主蘭垡堡蘭一ABSTRACTDYNAMICCHARACTERISTICSOFAEROENGINEPARTSAFL’ECTAER0一ENGINC’SPERFORMANCEANDSECURITYGREATLYTHEREFOREDAMAGEDIAGNOSIS,、】HICHINBASEDONEXPERIMENTALMODALANALYSISPARAMETERSONAEMENGINEPANS,ISASIGILIFICATIVEANDPROMISINGMETHODAMECHA“CALSTRUCTURECANBESTRUCTLLREDBYMASS,RIGIDITYAILDDAMPMATRIXESSYSTE肌WHENEVERDAⅡLAGEH印PENED,EVERYMATRIXESLIBECHANGEDEXC印TMASSMATRIX,WHICHLEADSTOMODALP猢ETERCHANGEDINSOMEWAYS,也ECHANGESOFMODALPARAMETERSEQUALSTOTHED啪AGEOFSTRUCTURCEXPE“MENTALMODALANALYSISISASYSTEMIDENTI矗CATIONPROCESS,WHICHISBASEDONLINEAFVIBMTIONTHEORY,DYNAMICTESTTECHLLOLOGY,DIGITALSJGNALPROCESSANDPARAMETERIDEM確CATIONTHEAUTHORDOTHE仃ADITIONALA11ALYSISONSECONDTURBINEPLATE,AILDGET“SNATLLRALFREQUENCYANDSHAPEOFEACHMODEIT’STHEBASISOFDYNAMICDESIGNANDNLODIFICATION,WITHTHEHELPOFFORRILEREXPERIMENTS,THEAUTLLORSTUDYMED鋤AGEIDEM訪CATIONMETHODONTHEEXPERIMENTAIANALYSISPARAMETERSANDNEILRALNETT001THEDIAGNOSISSYMBOLISMADEUPOFMODALSH印E,MODALFKQUENCYA11DMEIRCOMBINATIONANDATLAS“T’SPROVEDTHATTHEDAMAGEDIAGNOSISOFAEMENGINEPARTS,WHICHISBASEDONEXPERIMENTA】NLODALANALYSISA玎DITSPARAMETERISAVAILABLEKEYWORDEMAEXPERIMENTALMODALANALYSISEXPERIMENTALMODALPARAMETERDAMAGEIDENTIFICATIONIL
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簡(jiǎn)介:論文題目航空發(fā)動(dòng)機(jī)低壓渦輪葉片疲勞壽命預(yù)測(cè)學(xué)科專業(yè)機(jī)械工程學(xué)號(hào)201321080103作者姓名尹珩蘇指導(dǎo)教師黃洪鐘教授FATIGUELIFEPREDICTIONOFLOWPRESSURETURBINEBLADEOFAEROENGINEAMASTERTHESISSUBMITTEDTOUNIVERSITYOFELECTRONICSCIENCEANDTECHNOLOGYOFCHINAMAJORMECHANICALENGINEERINGAUTHORHENGSUYINSUPERVISORPROFHONGZHONGHUANGSCHOOLSCHOOLOFMECHATRONICSENGINEERING
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簡(jiǎn)介:分類號(hào)分類號(hào)TPTPTPTP273273273273密級(jí)級(jí)公開(kāi)UDCUDCUDCUDC單位代碼單位代碼10424104241042410424學(xué)位論文基于基于PC/104PC/104PC/104PC/104的輕小型的輕小型航空遙感系統(tǒng)航空遙感系統(tǒng)集成的集成的研究研究李紹剛申請(qǐng)學(xué)位級(jí)別申請(qǐng)學(xué)位級(jí)別碩士學(xué)位碩士學(xué)位專業(yè)專業(yè)名稱稱控制理論與控制工控制理論與控制工程指導(dǎo)教師姓名指導(dǎo)教師姓名陶安利職稱稱教授山東科技大學(xué)二零壹壹年五月二零壹壹年五月THETHERESEARCHRESEARCHOFOFLIGHTIGHTSMALLSMALLAVIATIONAVIATIONREMOTEREMOTESENSINGSENSINGSYSTEMSYSTEMINTEGRATIONINTEGRATIONBASEDASEDONONPCPC/104104AAAADISSERTATIONDISSERTATIONDISSERTATIONDISSERTATIONSUBMITTEDSUBMITTEDSUBMITTEDSUBMITTEDININININFULFILLMENTFULFILLMENTFULFILLMENTFULFILLMENTOFOFOFOFTHETHETHETHEREQUIREMENTSREQUIREMENTSREQUIREMENTSREQUIREMENTSFORFORFORFORTHETHETHETHEDEGREEDEGREEDEGREEDEGREEOFOFOFOFMASTERMASTERMASTERMASTEROFOFOFOFPHILOSOPHYPHILOSOPHYPHILOSOPHYPHILOSOPHYFROMFROMFROMFROMSHANDONGSHANDONGSHANDONGSHANDONGUNIVERSITYUNIVERSITYUNIVERSITYUNIVERSITYOFOFOFOFSCIENCESCIENCESCIENCESCIENCEANDANDANDANDTECHNOLOGYTECHNOLOGYTECHNOLOGYTECHNOLOGYBYBYBYBYLILILILISHAOGANGSHAOGANGSHAOGANGSHAOGANGSUPERVISORSUPERVISORSUPERVISORSUPERVISORPROFESSORPROFESSORPROFESSORPROFESSORTAOTAOTAOTAOANLIANLIANLIANLICOLLEGECOLLEGECOLLEGECOLLEGEOFOFOFOFINFORMATIONINFORMATIONINFORMATIONINFORMATIONANDANDANDANDELECTRICALELECTRICALELECTRICALELECTRICALENGINEERINGENGINEERINGENGINEERINGENGINEERINGMAYMAYMAYMAY2012012012011111
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簡(jiǎn)介:分類號(hào)學(xué)號(hào)M200971181學(xué)校代碼10487密級(jí)碩士學(xué)位論文碩士學(xué)位論文航天繼電器航天繼電器瞬態(tài)粘連特性瞬態(tài)粘連特性研究研究學(xué)位申請(qǐng)人學(xué)位申請(qǐng)人劉明澤劉明澤學(xué)科專業(yè)學(xué)科專業(yè)高電壓與絕緣技術(shù)高電壓與絕緣技術(shù)指導(dǎo)教師指導(dǎo)教師李震彪李震彪教授教授答辯日期答辯日期2012年1月6號(hào)獨(dú)創(chuàng)性聲明本人聲明所呈交的學(xué)位論文是我個(gè)人在導(dǎo)師指導(dǎo)下進(jìn)行的研究工作及取得的研究成果。盡我所知,除文中已經(jīng)標(biāo)明引用的內(nèi)容外,本論文不包含任何其他個(gè)人或集體已經(jīng)發(fā)表或撰寫過(guò)的研究成果。對(duì)本文的研究做出貢獻(xiàn)的個(gè)人和集體,均已在文中以明確方式標(biāo)明。本人完全意識(shí)到本聲明的法律結(jié)果由本人承擔(dān)。學(xué)位論文作者簽名年月日學(xué)位論文版權(quán)使用授權(quán)書學(xué)位論文版權(quán)使用授權(quán)書本學(xué)位論文作者完全了解學(xué)校有關(guān)保留、使用學(xué)位論文的規(guī)定,即學(xué)校有權(quán)保留并向國(guó)家有關(guān)部門或機(jī)構(gòu)送交論文的復(fù)印件和電子版,允許論文被查閱和借閱。本人授權(quán)華中科技大學(xué)可以將本學(xué)位論文的全部或部分內(nèi)容編入有關(guān)數(shù)據(jù)庫(kù)進(jìn)行檢索,可以采用影印、縮印或掃描等復(fù)制手段保存和匯編本學(xué)位論文。本論文屬于保密□,在年解密后適用本授權(quán)書。不保密□。(請(qǐng)?jiān)谝陨戏娇騼?nèi)打“√”)學(xué)位論文作者簽名指導(dǎo)教師簽名年月日年月日
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簡(jiǎn)介:西北工業(yè)大學(xué)碩士學(xué)位論文基于UG的航空發(fā)動(dòng)機(jī)零件夾具CAD系統(tǒng)研制姓名朱曉嬋申請(qǐng)學(xué)位級(jí)別碩士專業(yè)航空工程指導(dǎo)教師李建華張耦耕20051201西北工業(yè)大學(xué)T程碩十學(xué)位論文摘要ABSTRACTTHEDESIGNINGANDMANUFACTURINGOFFIXTUREISAVERYIMPORTANTPROCESSINTHECYCLEOFAEROENGINEMANUFACTURING.THEQUALITYOFFIXTUREDESIGNINGANDMANUFACTURINGISTHEKEYTOENSNL℃THEQUALITYOFPARTS,ANDTHECYCLEOFFIXTUREDESIGNINGANDMANUFACTURINGDECIDETHECYCLEOFPRODUCTIONPREPARATIORLTHISPAPCRMAINLYINTRODUCEDTHEDEVELOPMENTOFTHEUGSOT【W(wǎng)AREFORTHEAPPLICATIONOFTHEAEROENGINEPARTSFIXTUREDESIGNING,ANDONTHEFOUNDATIONOFTHEINVESTIGATION,THEAUTHORBUILTAFIXTUREDESIGNINGCADSYSTEMBASEDONUGSOFTWARE.INTHISPROCESSTHEAUTHORHASDONEMANYWORKSINVESTIGATEDTHEDEVELOPEDTECHNIQUEOFTHEUGSORWARE,ANDHASWRITTENSOMEPROGRAMSFORTHESYSTEM;INVESTIGATEDTHEMETHODFORDEVELOPINGSTANDARD/COMMONUSEDPARTSLIBRARY,BUILTTHEEXPANDABLESTANDARD/COMMONUSEDPARTSLIBRARY.THEAUTHORINVESTIGATEDTHEAPPLICATIONOFCASEBASEDDESIGNMETHODABOUTTHEFIXTUREDESIGNING.ANDBUILTTHEINSTANCELIBRARYOFTYPICALFIXTUREWHICHISINSTANCEDBYTHEAEROENGINEBLADEFIXTUREDESIGNING.ATLAST,THEAUTHORBUILTTHEUGDRANINGTEMPLATES,WHICHLAIDTHEFOUNDATIONSFORTHERESEARCHANDAPPLICATIONOFCADFORAEFOENGINETOOLDESIGNING.KEYWORDSCAD,F(xiàn)IXTURE,ASTANDARDPARTSLIBRARY,CASEBASEDDESIGN,ORANINGN
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簡(jiǎn)介:博士學(xué)位論文博士學(xué)位論文航天器自主交會(huì)對(duì)接制導(dǎo)與控制方法研究GUIDANCEANDCONTROLFORAUTONOMOUSRENDEZVOUSANDDOCKINGOFSPACECRAFT張大偉張大偉2010年12月CLASSIFIEDINDEXV4482UDC623DISSERTATIONFORTHEDOCTORALDEGREEINENGINEERINGGUIDANCEANDCONTROLFORAUTONOMOUSRENDEZVOUSANDDOCKINGOFSPACECRAFTCANDIDATEZHANGDAWEISUPERVISORPROFPEIRUNASSOCIATESUPERVISORPROFSONGSHENMINACADEMICDEGREEAPPLIEDFORDOCTOROFENGINEERINGSPECIALITYCONTROLSCIENCEANDENGINEERINGAFFILIATIONSCHOOLOFASTRONAUTICSDATEOFDEFENCEDECEMBER,2010DEGREECONFERRINGINSTITUTIONHARBININSTITUTEOFTECHNOLOGY
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簡(jiǎn)介:分類號(hào)UDC密級(jí)學(xué)位論文航天器在軌可更換模塊設(shè)計(jì)與分析作者姓名楊惠欣指導(dǎo)教師李樹(shù)軍教授東北大學(xué)機(jī)械工程與自動(dòng)化學(xué)院指導(dǎo)教師劉金國(guó)研究員中國(guó)科學(xué)院沈陽(yáng)自動(dòng)化研究所申請(qǐng)學(xué)位級(jí)別碩士學(xué)科類別工學(xué)學(xué)科專業(yè)名稱機(jī)械設(shè)計(jì)及理論論文提交日期2011年6月論文答辯日期2011年6月學(xué)位授予日期2011年7月答髓剩影妻主席翻、如不杪評(píng)閱人規(guī)KJ喲智眈里東北大學(xué)2011年6月獨(dú)創(chuàng)性聲明本人聲明,所呈交的學(xué)位論文是在導(dǎo)師的指導(dǎo)下完成的。論文中取得的研究成果除加以標(biāo)注和致謝的地方外,不包含其他人己經(jīng)發(fā)表或撰寫過(guò)的研究成果,也不包括本人為獲得其他學(xué)位而使用過(guò)的材料。與我一同工作的同志對(duì)本研究所做的任何貢獻(xiàn)均己在論文中作了明確的說(shuō)明并表示謝也思0學(xué)位論文作者簽名辛泓日期似糾彩銘學(xué)位論文版權(quán)使用授權(quán)書本學(xué)位論文作者和指導(dǎo)教師完全了解東北大學(xué)有關(guān)保留、使用學(xué)位論文的規(guī)定即學(xué)校有權(quán)保留并向國(guó)家有關(guān)部門或機(jī)構(gòu)送交論文的復(fù)印件和磁盤,允許論文被查閱和借閱。本人同意東北大學(xué)可以將學(xué)位論文的全部或部分內(nèi)容編入有關(guān)數(shù)據(jù)庫(kù)進(jìn)行檢索、交流。作者和導(dǎo)師同意網(wǎng)上交流的時(shí)間為作者獲得學(xué)位后半年口一年口一年半口兩年影學(xué)位論文作者等名一井物耄吹導(dǎo)師簽名簽字日期劬別OT、傭、簽字日期
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