o:18844 Синтеза тактичких ракета земља-ваздух против циљева великих брзина докторска дисертација Synthesis of tactical surface to air missile against high speed targets : doctoral dissertation 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... 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. Машинство-Војно машинство-Системи наоружања, ракетни системи / Mechanical engineering Scientific subdiscipline: Military engineering - Weapon systems, Missile systems Datum odbrane: 25. 9. 2018. пројектовање вођених ракета, аеродинамика, вођење и управљање, експлозивно формирани пројектили, нелинеарна симулација, ракетни погон, динамика лета missile design, aerodynamics, guidance and control, explosively formedprojectile, nonlinear simulation, propulsion, flight dynamics yes 514974115 91552101 6238 91552100 514974115 2018-11-28T12:13:09.053Z 45 no 46 mentor Miloš Д., 1987- Marković 2018 63 mentor Momčilo, 1954- Milinović 2018 63 član komisije Slobodan, 1952- Jaramaz 2018 63 član komisije Dejan, 1955- Micković 2018 63 član komisije Predrag, 1972- Elek 2018 63 član komisije Darko. Vasiljević 2018 XXI, 190 листова 19387118 http://phaidrabg.bg.ac.rs/o:18844 no yes 4 2018-11-28T12:13:09.320Z 70 11 1067197 1067418 пројектовање вођених ракета, аеродинамика, вођење и управљање, експлозивно формирани пројектили, нелинеарна симулација, ракетни погон, динамика лета missile design, aerodynamics, guidance and control, explosively formedprojectile, nonlinear simulation, propulsion, flight dynamics 623.462.2.027:623.465(043.3) 1738 11A30 2018