Show simple item record

MLRS salvo simulation

dc.creatorHolclajtner, Marko S.
dc.creatorJeremić, Olivera
dc.creatorMilinović, Momčilo
dc.date.accessioned2022-09-19T16:27:24Z
dc.date.available2022-09-19T16:27:24Z
dc.date.issued2010
dc.identifier.issn0042-8469
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/1057
dc.description.abstractU radu je predstavljena procedura za efikasno simuliranje rafala višecevnog bacača raketa i uticaja rakete na ostale delove sistema. Analizirano je ponašanje rakete u odnosu na referentnu idealnu trajektoriju, koju generiše idealna raketa. Kvalitet rafalne vatre je rasturanje padnih tačaka na cilju što je mera preciznosti i tačnosti. U radu je razmatran samo uticaj preciznosti, tj. rasturanja raketa, pri čemu se smatra da je greška tačnosti zanemarljiva. Na taj način identifikuju se sopstveni (municijski) uticaji na fenomen rasturanja trajektorija. Rasturanje na cilju upoređeno je sa rasturanjem na kraju aktivne faze u takozvanim estimatorskim koordinatama (detektorskoj ravni) i biće utvrđena njihova korelacija.sr
dc.description.abstractThis paper presents a procedure for an efficient simulation of MLRS barrage fire as well as of the effects of rocket parameters. The rocket behavior will be analyzed with reference to an ideal trajectory generated by an ideal rocket. The quality of MLRS fire is expressed through dispersion of impact points in the target area thus representing precision and accuracy. This work assumes absolutely correct accuracy and concentrates primarily on the effects of precision i. e. on the dispersion of rockets. Other types of effects on rocket dispersion, such as those of atmosphere, launching, etc. are neglected. The ammunition effects on the trajectory dispersion will be thus identified. The dispersion in the target area will be correlated with the dispersion of trajectory points at the end of the active (rocket motor burn out) phase.en
dc.publisherUniverzitet odbrane u Beogradu - Institut za naučne informacije, Beograd
dc.relationinfo:eu-repo/grantAgreement/MESTD/MPN2006-2010/14062/RS//
dc.rightsopenAccess
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.sourceVojnotehnički glasnik
dc.subjectslučajna odstupanjasr
dc.subjectrealna raketasr
dc.subjectrasturanje na ciljusr
dc.subjectnumerička simulacijasr
dc.subjectidealna raketasr
dc.subjectekscentar potiskasr
dc.subjectdinamika letasr
dc.subjectdinamički ekscentarsr
dc.subjectaktivna fazasr
dc.subjecttrust misalignmenten
dc.subjectreal rocketen
dc.subjectrandom deviationen
dc.subjectnumerical simulationen
dc.subjectidealised rocketen
dc.subjectflight mechanicsen
dc.subjectdynamic misalignmenten
dc.subjectdispersion in the target areaen
dc.subjectactive phaseen
dc.titleSimulacija rafala višecevnog bacača raketasr
dc.titleMLRS salvo simulationen
dc.typearticle
dc.rights.licenseBY
dc.citation.epage25
dc.citation.issue2
dc.citation.other58(2): 5-25
dc.citation.rankM53
dc.citation.spage5
dc.citation.volume58
dc.identifier.doi10.5937/vojtehg1002005H
dc.identifier.fulltexthttp://machinery.mas.bg.ac.rs/bitstream/id/36/1054.pdf
dc.type.versionpublishedVersion


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record