Simulacija leta tenkovskog projektila

undergraduate thesis

• Title (english): Flight Simulation of Tank Projectile
• Author: Kristian Blažević
• Mentor: Milan Vrdoljak (mentor)
• Mentor: Zvonko Trzun (mentor)
• Committee member: Milan Vrdoljak (predsjednik povjerenstva)
• Committee member: Dario Matika (član povjerenstva)
• Committee member: Zvonko Trzun (član povjerenstva)
• Committee member: Dario Zlatar (član povjerenstva)
• Granter: University of Zagreb; (Croatian Defence Academy "Dr. Franjo Tuđman"); Zagreb
• Defense date and country: 2018-09-11, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Interdisciplinary Technical Sciences

Abstract

Cilj ovog završnog rada je prikazati potrebu za korištenjem modela leta u uspješnom djelovanju iz tenkovskog topa. Modeli leta su matematički modeli koji uzimaju u obzir sve elemente okoline i sustava projektila kako bi što točnije predvidjeli parametre leta projektila. Iz tog razloga provode se simulacije leta tenkovskih projektila kako bi tenk uspješno djelovao na terenu iz tenkovskog topa. Naziv ovog rada je Simulacija leta tenkovskog projektila jer se u njemu iznose bitni podatci o tenku iz kojeg se gađa, projektilu čiji let simuliramo i osnovne pretpostavke modela pomoću kojeg simuliramo let. U radu je provedena analiza utjecaja vjetra na putanju i domet projektila te su rezultati prikazani grafički.

Abstract (english)

The goal of this bachelor thesis is to show the need of using correct flight model in succesfull action from tank cannon. Flight models are mathematical model which take in consideration all elements of the environment and projectile system to predict, as much as accurate, parameters of projectile flight. For that reason, tank projectile flight simulations are conducted so that tank could succsessfully act form his cannon in the field. The title of this thesis is Flight simulation of tank projectile because here are stated important data about the tank that's firing the projectile, projectile which flight we simulate and basic assumptions of the model we are using to simulate the flight. In this thesis the analysis of the wind influence on trajectory and range was carried out and the results where displayed graphically.

• Keywords: model leta; tenkovski top; tenkovski projektili; putanja; domet
• Keywords (english): flight model; tank cannon; tank projectiles; trajectory; range
• Language: croatian
• URN:NBN: urn:nbn:hr:249:692271
• Study programme: Title: Military Engineering; Study programme type: university; Study level: undergraduate; Academic / professional title: sveučilišni/a prvostupnik/ prvostupnica inženjer/inženjerka vojnog inženjerstva (sveučilišni/a prvostupnik/ prvostupnica inženjer/inženjerka vojnog inženjerstva)
• Type of resource: Text
• File origin: Born digital
• Access conditions: Closed access
• Created on: 2019-10-25 08:29:38