2、025)摘要：為提高導(dǎo)彈武器系統(tǒng)的生存能力和快速反應(yīng)能力，對導(dǎo)彈起豎過程中的對地荷載進(jìn)行研究。分析在導(dǎo)彈起豎過程中發(fā)射場坪所受載荷，將發(fā)射車視為左右對稱體，在考慮風(fēng)載荷影響的前提下，計(jì)算出導(dǎo)彈起豎過程中的前后支腿對地壓力，為建立發(fā)射場坪的評估模型提供了載荷判據(jù)；利用壓力檢測裝置采集導(dǎo)彈起豎時(shí)的支腿對地壓力，得到了支腿壓力隨起豎角度的變化曲線，并以現(xiàn)場實(shí)測進(jìn)行數(shù)據(jù)采集結(jié)果分析。分析結(jié)果表明：理論計(jì)算結(jié)果和壓力幅值與變化趨勢較為吻合，計(jì)算結(jié)果合理，可為導(dǎo)彈無依托發(fā)射的場坪選取和判斷提供參考。關(guān)鍵詞：無依托發(fā)射；承載能力；載荷
3、分析StudyontheLoadtoGroundonMissileErectionProcessChengHongjic1,QianZhibo1,ZhaoYuan2,LiBinmao1(1.CollegeofMarine,NorthwesternPolytechnicalUniversity,Xi'an710072,China)(2.Depl.ofBasicTheories,SecondArtilleryEngineeringCollege,Xi'an710025,China)Abstract:Toenhancethes
4、urvivalcapabilityandfastreactioncapabilityofmissileweaponsystem,studyontheloadtogroundduringtheprocessofmissileerectionhasbeencarriedout.Thebearingloadoflaunchingsiteisanalyzedinmissileerectingprocesswiththehypothesisthatthelaunchingvehicleisbilateralsymmetryobje
5、ct,andjackreactionforceinerectingprocessiscalculatedwhiletheinfluenceofwindloadisconsidered,whichprovidesloadcriterionforbuildingevaluationmodeloflaunchingsite?Therunningcurveofjackreactionforcerelatedtoerectingangleisyieldedthroughusingpressu『edataacquisitionsys
6、tem,andthedataacquisitionresultisanalyzedwithrealmeasuringdata?Theanalyzedresultshowsthatamplitudeandvariationtrendofjacksreactionforcearcinwellmatchwiththeoreticalcalculationresults,andthecomputationresultisrational,whichcanofferreferencesforselectingandjudgingi
7、ntensityofmissilelaunchingsitewhenunsupportedrandomlaunchingwayisapplied?Keywords:unsupportedrandomlaunching;bearingcapacity;loadanalysisrTwrTwrjwrYwrYwrTwrYw?Tw?TwrTwrTwrTwrTwrTwrYw?Tw?TwrTwrTwrTwrTwrYwrTwrTwrYwrTwrTwrTwrTwrYw?Tw?Tw反艦作戰(zhàn)中的反輻射導(dǎo)彈運(yùn)用優(yōu)化王肖飛I，嚴(yán)建鋼2,趙杰I,袁
8、有宏*(1.海軍航空工程學(xué)院研究生大隊(duì)，山東煙臺264001；2.海軍航空工程學(xué)院指揮系，山東煙臺264001)摘要：為研究反輻射導(dǎo)彈在反艦作戰(zhàn)中與常規(guī)反艦導(dǎo)彈的協(xié)同運(yùn)用效果，建立了反艦導(dǎo)彈的突防概率模型，在反輻射導(dǎo)彈對艦艇防空雷達(dá)的毀傷概率研究基礎(chǔ)上，建立反輻射導(dǎo)彈對搜索雷達(dá)、制導(dǎo)雷達(dá)和炮瞄雷達(dá)的毀傷模型，仿真在不
