Sinteza taktičkih raketa zemlja-vazduh protiv ciljeva velikih brzina
Synthesis of tactical surface to air missile against high speed targets
2018
Аутори
Marković, MilošОстала ауторства
Milinović, MomčiloJaramaz, Slobodan
Micković, Dejan
Elek, Predrag
Vasiljević, Darko
Докторска теза (Објављена верзија)
Метаподаци
Приказ свих података о документуАпстракт
U radu je predstavljen integralni pristup istraživanju parametara projektovanja raketa sa aspekta usaglašavanja ograničenja proisteklih iz zadataka mehanike pri posebnim uslovima gađanja balističkih ciljeva koji nameću različite konstruktivne kompromise...
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 w...as 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.
Кључне речи:
vođenje i upravljanje / raketni pogon / projektovanje vođenih raketa / nelinearna simulacija / eksplozivno formirani projektili / dinamika leta / aerodinamika / propulsion / nonlinear simulation / missile design / guidance and control / flight dynamics / explosively formed projectile / aerodynamicsИзвор:
2018Издавач:
- Univerzitet u Beogradu, Mašinski fakultet
Финансирање / пројекти:
- Рентабилни избор нових технологија и концепција одбране кроз друштвене промене и стратешке оријентације Србије у 21. веку (RS-MESTD-Integrated and Interdisciplinary Research (IIR or III)-47029)
URI
http://eteze.bg.ac.rs/application/showtheses?thesesId=6238https://nardus.mpn.gov.rs/handle/123456789/10206
https://fedorabg.bg.ac.rs/fedora/get/o:18844/bdef:Content/download
http://vbs.rs/scripts/cobiss?command=DISPLAY&base=70036&RID=514974115
https://machinery.mas.bg.ac.rs/handle/123456789/57
Колекције
Институција/група
Mašinski fakultetTY - THES AU - Marković, Miloš PY - 2018 UR - http://eteze.bg.ac.rs/application/showtheses?thesesId=6238 UR - https://nardus.mpn.gov.rs/handle/123456789/10206 UR - https://fedorabg.bg.ac.rs/fedora/get/o:18844/bdef:Content/download UR - http://vbs.rs/scripts/cobiss?command=DISPLAY&base=70036&RID=514974115 UR - https://machinery.mas.bg.ac.rs/handle/123456789/57 AB - U radu je predstavljen integralni pristup istraživanju parametara projektovanja raketa sa aspekta usaglašavanja ograničenja proisteklih iz zadataka mehanike pri posebnim uslovima gađanja balističkih ciljeva koji nameću različite konstruktivne kompromise... AB - 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. PB - Univerzitet u Beogradu, Mašinski fakultet T1 - Sinteza taktičkih raketa zemlja-vazduh protiv ciljeva velikih brzina T1 - Synthesis of tactical surface to air missile against high speed targets UR - https://hdl.handle.net/21.15107/rcub_nardus_10206 ER -
@phdthesis{ author = "Marković, Miloš", year = "2018", abstract = "U radu je predstavljen integralni pristup istraživanju parametara projektovanja raketa sa aspekta usaglašavanja ograničenja proisteklih iz zadataka mehanike pri posebnim uslovima gađanja balističkih ciljeva koji nameću različite konstruktivne kompromise..., 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.", publisher = "Univerzitet u Beogradu, Mašinski fakultet", title = "Sinteza taktičkih raketa zemlja-vazduh protiv ciljeva velikih brzina, Synthesis of tactical surface to air missile against high speed targets", url = "https://hdl.handle.net/21.15107/rcub_nardus_10206" }
Marković, M.. (2018). Sinteza taktičkih raketa zemlja-vazduh protiv ciljeva velikih brzina. Univerzitet u Beogradu, Mašinski fakultet.. https://hdl.handle.net/21.15107/rcub_nardus_10206
Marković M. Sinteza taktičkih raketa zemlja-vazduh protiv ciljeva velikih brzina. 2018;. https://hdl.handle.net/21.15107/rcub_nardus_10206 .
Marković, Miloš, "Sinteza taktičkih raketa zemlja-vazduh protiv ciljeva velikih brzina" (2018), https://hdl.handle.net/21.15107/rcub_nardus_10206 .