Приказ основних података о документу
Zone zahvata raketama u proporcionalno navođenom letu sa vazdušno reaktivnim pogonom
Engagement areas of missiles in the proportional navigated flight powered by air breathing engines
dc.creator | Marković, Miloš | |
dc.creator | Rašuo, Boško | |
dc.creator | Milinović, Momčilo | |
dc.creator | Amine, Mohammed Boulahlib | |
dc.date.accessioned | 2022-09-19T17:30:06Z | |
dc.date.available | 2022-09-19T17:30:06Z | |
dc.date.issued | 2014 | |
dc.identifier.issn | 1451-2092 | |
dc.identifier.uri | https://machinery.mas.bg.ac.rs/handle/123456789/1974 | |
dc.description.abstract | Ciljevi ovog iztraživanja su testiranje odnosa odgovarajućih letnih performansi posredno upravljanih raketa i uslovno kreiranje njihovih taktičkih, prostornih zona i vremena gađanja tokom upotrebe na površinske ciljeve. Manevar leta, posredno daljinski upravljane rakete je testiran sa uslovno povezanim ograničenjima koja proističu iz kinematike leta sa turbomlaznim pogonom rakete i načina kretanja cilja, tipičnog za iznenadne napade. Ograničenja sposobnosti manervisanja u letu, u fazi krstarenja, su razmatrani kao modeli kretanja materijalne tačke radi kreiranja nevođenih (pretraživanja) i vođenih navigacionih kinematskih trajektorija, projektovanih po odgovarajućem zakonu navigacije. U iztraživanju je korišćen numerički metod za simuliranje kretanja posredno upravljane rakete i cilja u horizontalnoj ravni kontrolisanjem linije cilja na odgovarajućoj visini leta. Ovo generiše granice zone pogotka i zone lansiranja, uspostavljene pomoću operativnog vremena leta posredno vođenih raketa kao i mogućih varijacija mase za očekivani način borbenog leta. | sr |
dc.description.abstract | The goals of this research are to test the relationships of appropriate nonline of site (NLOS) missile flight performances and conditionally created their tactical ranges, spaces zones and shooting time during employment on the surface targets. Flight maneuver of distance remote controlled NLOS missile is tested with the conditionally joint constrains coming from flight kinematics with turbo-jet engine of NLOS missile and manner of target motion, typical of rapid reaction attacks. The constraints of maneuverability and flight, in the cruise phase, are considered as the mass point motion to create both unguided (searching) and guided navigated kinematical trajectories, which was designed by the appropriate guidance law. Research used numerical methods to simulate NLOS missile and targets motions in horizontal plane by controlling line of target (LOT) referred at the appropriate flight height. This generates borders of target impact and launching areas, establishes NLOS missile operation time, as well as masses variations for the expected manner of battle flight. . | en |
dc.publisher | Univerzitet u Beogradu - Mašinski fakultet, Beograd | |
dc.relation | info:eu-repo/grantAgreement/MESTD/Integrated and Interdisciplinary Research (IIR or III)/47029/RS// | |
dc.rights | openAccess | |
dc.rights.uri | https://creativecommons.org/licenses/by/4.0/ | |
dc.source | FME Transactions | |
dc.subject | shooting area | en |
dc.subject | range performances | en |
dc.subject | proportional navigation | en |
dc.subject | non-line of site missile | en |
dc.subject | endurance of flight | en |
dc.title | Zone zahvata raketama u proporcionalno navođenom letu sa vazdušno reaktivnim pogonom | sr |
dc.title | Engagement areas of missiles in the proportional navigated flight powered by air breathing engines | en |
dc.type | article | |
dc.rights.license | BY | |
dc.citation.epage | 188 | |
dc.citation.issue | 3 | |
dc.citation.other | 42(3): 181-188 | |
dc.citation.rank | M24 | |
dc.citation.spage | 181 | |
dc.citation.volume | 42 | |
dc.identifier.doi | 10.5937/fmet1403181M | |
dc.identifier.fulltext | http://machinery.mas.bg.ac.rs/bitstream/id/776/1971.pdf | |
dc.identifier.scopus | 2-s2.0-84905907188 | |
dc.type.version | publishedVersion |