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Synthesis of tactical surface to air missile against high speed targets

dc.contributor.advisorMilinović, Momčilo
dc.contributor.otherJaramaz, Slobodan
dc.contributor.otherMicković, Dejan
dc.contributor.otherElek, Predrag
dc.contributor.otherVasiljević, Darko
dc.creatorMarković, Miloš Д.
dc.date.accessioned2018-11-30T16:40:14Z
dc.date.available2018-11-30T16:40:14Z
dc.date.available2020-07-03T08:43:58Z
dc.date.issued2018-09-24
dc.identifier.urihttps://nardus.mpn.gov.rs/handle/123456789/10206
dc.identifier.urihttp://eteze.bg.ac.rs/application/showtheses?thesesId=6238
dc.identifier.urihttps://fedorabg.bg.ac.rs/fedora/get/o:18844/bdef:Content/download
dc.identifier.urihttp://vbs.rs/scripts/cobiss?command=DISPLAY&base=70036&RID=514974115
dc.description.abstractУ раду је представљен интегрални приступ истраживању параметара пројектовања ракета са аспекта усаглашавања ограничења проистеклих из задатака механике при посебним условима гађања балистичких циљева који намећу различите конструктивне компромисе...sr
dc.description.abstractAn integral approach has been presented on the research of missile design parameters from the aspect of harmonizing the limitations arising from the tasks of mechanics under the special conditions of hiting ballistic targets that impose various constructive compromises. Shooting target was analyzed for the most complex procedure of defense against ballistic targets. Basis on previous, it was establish criteria for require missile impact parameters and its ideal limit capabilities. The required normal acceleration, miss distance and control effort for each of the threshold missions are estimated. Based on the established criteria, a further aerodynamic design procedure is given, which is manifested through the selection of body geometric and aerodynamic performances, as well as appropriate control concepts for the requirements of the required maximum normal acceleration in the conditions of threshold flight missions. The synthesis of the autopilot of the vertical launch of the missile was performed, as well as the determination performances of the selected type of thrust vector control system and aerodynmaics for the purpose of hybrid control analysis. In particular, the propulsion performance assessment was carried out to integrate total flight and impact assessment of axial acceleration during the initial phase after vertical launch. The results of the influence parameters on the dynamic characteristics of the vertical launch of the missile in the active phase for hybrid control are presented. A mathematical model of possible use of a warhead for direct hit by an explosive-formed projectile was performed. Design approach and application of explosively-formed projectiles is presented as a potential useful warhead based on the adopted analytical and numerical methods.en
dc.formatapplication/pdf
dc.languagesr
dc.publisherУниверзитет у Београду, Машински факултетsr
dc.relationinfo:eu-repo/grantAgreement/MESTD/Integrated and Interdisciplinary Research (IIR or III)/47029/RS//
dc.rightsopenAccessen
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/
dc.sourceУниверзитет у Београдуsr
dc.subjectпројектовање вођених ракетаsr
dc.subjectmissile designen
dc.subjectaerodynamicsen
dc.subjectguidance and controlen
dc.subjectexplosively formed projectileen
dc.subjectnonlinear simulationen
dc.subjectpropulsionen
dc.subjectflight dynamicsen
dc.subjectаеродинамикаsr
dc.subjectвођење и управљањеsr
dc.subjectексплозивно формирани пројектилиsr
dc.subjectнелинеарна симулацијаsr
dc.subjectракетни погонsr
dc.subjectдинамика летаsr
dc.titleСинтеза тактичких ракета земља-ваздух против циљева великих брзинаsr
dc.title.alternativeSynthesis of tactical surface to air missile against high speed targetsen
dc.typedoctoralThesisen
dc.rights.licenseBY-NC-ND
dc.identifier.fulltexthttp://nardus.mpn.gov.rs/bitstream/id/7832/Disertacija.pdf
dc.identifier.fulltexthttp://nardus.mpn.gov.rs/bitstream/id/7833/IzvestajKomisije18416.pdf
dc.identifier.fulltexthttps://nardus.mpn.gov.rs/bitstream/id/7832/Disertacija.pdf
dc.identifier.fulltexthttps://nardus.mpn.gov.rs/bitstream/id/7833/IzvestajKomisije18416.pdf
dc.identifier.rcubhttps://hdl.handle.net/21.15107/rcub_nardus_10206


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