diplomska naloga visokošolskega strokovnega študijskega programa I. stopnje strojništvo
Jakob Vojvoda (Author), Tadej Kosel (Mentor)

Abstract

Zaradi spremembe področja uporabe brezpilotnih letal Bramor podjetja C-Astral iz kopnega na morje, je potrebna zasnova novega pristajalnega sistema, ki bo omogočal učinkovito uporabo teh letal na novem področju. Gonilo razvoja novega sistem je predvidena uporaba letal Bramor s strani Slovenske vojske na ladji Triglav, kjer obstoječi pristajalni sistem letala (integrirano padalo) ni dovolj natančen za uporabo. Potrebna je torej zasnova novega pristajalnega sistema, ki omogoča natančne pristanke na prostorsko omejenem območju, ki ga predstavlja ladja. V začetku dela so predstavljene funkcijske in konstrukcijske omejitve sistema, preko katerih je oblikovan prvi koncept. Prvi koncept je v delu predstavljen z vidika konstrukcije in uporabe, podana pa je tudi ocena koncepta. V nadaljevanju je prvi koncept zaradi dodatnih zahtev preoblikovan v drugi koncept, ki je tako kot prvi predstavljen z vidika konstrukcije in uporabe. Tretji koncept je rezultat testiranj ter novih in spremenjenih zahtev. Tako kot prvi in drugi, je tretji koncept v začetku predstavljen z vidika konstrukcije in uporabe. V nadaljevanju dela je predstavljena tudi izvedba tretjega koncepta in uporabljenih elementov, ki predstavlja končno obliko sistema. Sistem je zasnovan tako, da zadosti vsem funkcijskim in konstrukcijskim zahtevam, je zanesljiv, enostaven za uporabo in zasnovan tako, da omogoča prilagajanje sistema na druga plovila.

Keywords

diplomske naloge;brezpilotni letalniki;brezpilotni sistemi;pristajalni sistemi;pristanki na plovila;pristanki s trki;varnostne mreže;

Data

Language: Slovenian
Year of publishing:
Typology: 2.11 - Undergraduate Thesis
Organization: UL FS - Faculty of Mechanical Engineering
Publisher: [J. Vojvoda]
UDC: 004.925.84:623.746-519(043.2)
COBISS: 16103963 Link will open in a new window
Views: 854
Downloads: 440
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Other data

Secondary language: English
Secondary title: Design of a landing system for catching of an unmanned airplane
Secondary abstract: Due to the change in the area of operation of C-Astral's Bramor unmanned airplanes from land to sea, a design of a new landing system is needed to allow efficient use of these aircraft in the new field. The development of the new system is mainly driven by the intended use of Bramor aircraft on Slovenian army vessel Triglav, where the existing landing system of the airplane (integrated parachute) is not sufficiently precise for use. It is therefore necessary to design a new landing system that allows precise landings in the spatially restricted area represented by the vessel. At the beginning of the work, the functional and structural constraints of the system are presented through which the first concept is designed. The first concept is than presented through structural components and use, and finally an evaluation of the concept is given. In the continuation, the first concept is transformed into the second concept due to additional new requirements, which were presented during design phase. Similarly to the first concept the second concept is presented in terms of construction elements and use. Finally the third concept is presented which is the result of tests and some new and changed requirements. Like the first and second concepts, it is initially presented through the point of view of construction elements and use. In the continuation of the work, the third concept is than presented through its elements as the final form of the system. The system is in its final form designed to satisfy all functional and constructional demands, it is reliable, easy to use, and designed in such a way that it allows certain modifications to be made to the system to adapt it to specific types of vessels.
Secondary keywords: unmanned aircrafts;unmanned systems;landing systems;landings on vessels;arrested landings;safety nets;
Type (COBISS): Bachelor thesis/paper
Study programme: 0
Embargo end date (OpenAIRE): 1970-01-01
Thesis comment: Univ. v Ljubljani, Fak. za strojništvo
Pages: XXII, 70 str.
ID: 10941550
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