[ 1 ] 朱安文, 曲广吉, 高耀南, 魏震松.结构动力模型修正技术的发展[J].力学进展, 2002, (8) :337～348 链接1

[ 2 ] CollinsJD, HartGC, HasselmanTK, KennedyB.Statisticalidentificationofstructures[J].AIAA Journal, 1974, 12 (2) :185～190

[ 3 ] PilkeyWD, CohenR.SystemIdentificationof VibratingStructures, MathematicalModelsfromTest Data[M].AmericanSocietyofMechanicalEngineers, NewYork, 1972

[ 4 ] HasselmanTK, ChrostowskiJD.Arecentcasestudy insystemidentification[A].AIAA$C91$C1190$CCP, Procof32ndAIAAStructures[C].Structural DynamicsandMaterialsConference, April1991.2154～2168

[ 5 ] DascotteE.Applicationsoffiniteelementmodaltuning usingexperimentalmodaldata[J].Soundand Vibration, 1991, 25 (6) :22～26

[ 6 ] ChenJC, GarbaJA.Analyticalmodelimprovement usingmodaltestresults[J].AIAAJournal, 1980, 18 (6) :684～690

[ 7 ] ChenJC, WadaBK.Matrixperturbationfor structuraldynamicanalysis[J].AIAAJournal, 1977, 15 (8) :1095～1100

[ 8 ] ChenJC, GarbaJA.On-orbitdamageassessment forlargespacestructures[J].AIAAJournal, 1988, 26 (9) :1119～1126

[ 9 ] MuralidharKV, ThomasKJ, BadariN, etal.Finite elementmodelimprovementsusingtestdata[J].JournalofSpacecraftTechnology, 2002, 12 (2) :14～24

[10] BermanA, FlannellyWG.Theoryofincomplete modelsofdynamicstructures[J].AIAAJournal, 1971, 9 (8) :1481～1487

[11] BaruchM, BarItzhackIY.Optimalweighted orthogonalizationofmeasuredmodes[J].AIAA Journal, 1978, 16 (4) :346～351

[12] BermanA, NagyEJ.Improvementofalarge analyticalmodalusingtestdata[J].AIAAJournal, 1983, 21 (8) :1168～1173

[13] KabeAM.Stiffnessmatrixadjustmentusingmode data[J].AIAAJournal, 1985, 23 (9) :1431～1436

[14] WeiFS.Massandstiffnessinteractioneffectsin analyticalmodelmodification[J].AIAAJournal, 1990, 28 (9) :1686～1688

[15] WeiFS.Analyticaldynamicmidelimprovementusing vibrationtestdata[J].AIAAJournal, 1990, 28 (1) :175～177

[16] ChouCM, O’CallahanJC, WuCH.Localizationof test/analysisstructuralmodelerrors[A].AIAA-89-1244-CP, 30thAIAAStructures[C].Structural DynamicsandMaterialsConference, April1989.748～752

[17] SrinivasK, KaoPJ, GeorgeW.Analysisandtest correlationofspacecraftstructuresusingdynamic parametersensitivities[A].AIAA-94-1502-CP, 35thAIAA/ASME/ASCE/AHS/ASCStructures[C].StructuralDynamicsandMaterialsConference, April1994.1475～1487

[18] ZhangDW, ZhangLM.Matrixtransformation methodforupdatingdynamicmodel[J].AIAA Journal, 1992, 30 (5) :1440～1443

[19] 张德文.利用广义逆变换修正动力模型[A].第四届全国振动理论及应用学术会议论文集[C].郑州, 1990.7～12

[20] 向锦武, 周传荣, 张阿舟.基于建模误差位置识别的有限元模型修正方法[J].振动工程学报, 1997, 10 (1) :1～6 链接1

[21] 李　书, 卓家寿, 任青文.动力模型总体修正的近似解析解[J].力学与实践, 1998, 20 (1) :37～39 链接1

[22] 张令弥, 何伯庆, 袁向荣.涉及灵敏度分析的迭代模态法[J].南京航空航天大学学报, 1994, 26 (3) :319～327 链接1

[23] 张景绘.动力学系统建模[M].北京:国防工业出版社, 2000 链接1

[24] 徐张明, 高天明, 沈荣瀛, 华宏星.一种改进的利用频响函数进行有限元模型修正的方法[J].振动与冲击, 2002, 21 (3) :43～46 链接1

[25] 徐张明, 沈荣瀛, 华宏星.基于频响函数相关性的灵敏度分析的有限元模型修正[J].机械强度, 2003, 25 (1) :5～8 链接1

[26] 秦仙蓉.基于灵敏度分析的结构计算模型修正及相关问题研究[D].南京航天航空大学, 2001

[27] HemezFM, BrownGW.Improvingstructural dynamicsmodelsbycorrelatingsimulatedtomeasured frequencyresponsefunctions[A].AIAA-98-1789, 39thAIAA/ASME/ASCE/AHS/ASCStructures[C].StructuralDynamicsandMaterialsConference, April1998.772～782

[28] TingT.Designsensitivityanalysisofstructural frequencyresponse[A].AIAA-92-4799-CP, 4th AIAA/USAF/NASA/OAISymposiumon MultidisciplinaryAnalysisandOptimization[C].Sept1992.878～881

[29] LinkM.Experiencewithdifferentproceduresfor updatingstructuralparametersofanalyticalmodels usingtestdata[A].Proceedingsofthe10th InternationalModalAnalysisConference[C].Sandiego, California, 1992.730～738