Title
Синтеза тактичких ракета земља-ваздух против циљева великих брзина
Creator
Marković, Miloš Д., 1987-
Copyright date
2018
Object Links
Select license
Autorstvo-Nekomercijalno-Bez prerade 3.0 Srbija (CC BY-NC-ND 3.0)
License description
Dozvoljavate samo preuzimanje i distribuciju dela, ako/dok se pravilno naznačava ime autora, bez ikakvih promena dela i bez prava komercijalnog korišćenja dela. Ova licenca je najstroža CC licenca. Osnovni opis Licence: http://creativecommons.org/licenses/by-nc-nd/3.0/rs/deed.sr_LATN. Sadržaj ugovora u celini: http://creativecommons.org/licenses/by-nc-nd/3.0/rs/legalcode.sr-Latn
Language
Serbian
Cobiss-ID
Theses Type
Doktorska disertacija
description
Datum odbrane: 25. 9. 2018.
Other responsibilities
mentor
Milinović, Momčilo, 1954-
član komisije
Jaramaz, Slobodan, 1952-
član komisije
Micković, Dejan, 1955-
član komisije
Elek, Predrag, 1972-
član komisije
Vasiljević, Darko.
Academic Expertise
Tehničko-tehnološke nauke
University
Univerzitet u Beogradu
Faculty
Mašinski fakultet
Alternative title
Synthesis of tactical surface to air missile against high speed targets
Publisher
[М. Д. Марковић]
Format
XXI, 190 листова
description
Машинство-Војно машинство-Системи наоружања, ракетни системи / Mechanical engineering
Scientific subdiscipline: Military engineering - Weapon systems, Missile systems
Abstract (sr)
У 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...
Abstract (en)
An 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.
Authors Key words
пројектовање вођених ракета, аеродинамика, вођење и управљање, експлозивно формирани пројектили, нелинеарна симулација, ракетни погон, динамика лета
Authors Key words
missile design, aerodynamics, guidance and control, explosively formed
projectile, nonlinear simulation, propulsion, flight dynamics
Classification
623.462.2.027:623.465(043.3)
Type
Tekst
Abstract (sr)
У 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...
“Data exchange” service offers individual users metadata transfer in several different formats. Citation formats are offered for transfers in texts as for the transfer into internet pages. Citation formats include permanent links that guarantee access to cited sources. For use are commonly structured metadata schemes : Dublin Core xml and ETUB-MS xml, local adaptation of international ETD-MS scheme intended for use in academic documents.