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A gallery of up-to-date and stylish LaTeX templates, examples to help you learn LaTeX, and papers and presentations published by our community. Search or browse below.

SWFU BSc thesis template
This template is for typesetting BSc thesis at Southwest Forestry University, Kunming, China.
You can always find the updated version at:
https://github.com/wx672/texmf/tree/master/doc/latex/swfu/swfcthesis/tutorial
Xiaolin WANG

Template onderzoekscompetenties 2017-2018 (6des)
Een template om het verslag van de onderzoekscompetenties in Overleaf te maken. Veel succes!
roeland vervenne

FH Aachen Mechanical Engineering Thesis Template
Beispiel für eine Bachelorarbeit mit FH Aachen FB 8
Titelblattstyles
Erstellt: Prof. Enning, 18.07.2013
Überarbeitet: Prof. Pfaff, 08.03.2018
Manfred Enning, Raphael Pfaff

Template of a Paper for NLA'2018 Conference
The article template for NLA'2018 conference. It is based on the standard llncs class (Lecture Notes in Computer Sciences) and adjusted with a style file of the conference. This Overleaf template contains two main files. One is for English papers and another for Russian ones. Switch templates via Overleaf Project menu. Conference site: http://nla.icc.ru/
Evgeny Cherkashin

Controle digital de um conversor CC-CC
Um artigo sobre controle digital de conversores CC-CC tipo buck utilizando microcontrolador STM cortex-m0+.
Ana Caroline Tondo Bonafim, Jefferson Willian França Góes, Raul Scarmosin Freitas

Template Boletin de Matematicas - 2018
This template is used as a basic template for the journal Boletín de Matemáticas, of the mathematics department of the Universidad Nacional de Colombia. More information can be found in the site of the journal
https://revistas.unal.edu.co/index.php/bolma
Boletin de Matemáticas

LaTeX: nem csak cikkekhez vagy dolgozatokhoz
Original: \(\mathrm{\LaTeX}\): More Than Just Academic Papers and Journals
Copyright Lim Lian Tze 2011-2018
Translation to Hungarian and extension by Erika Griechisch 2018
This work is licensed under a Creative Commons Attribution-NonCommercial-
ShareAlike 3.0 Unported License.
As this is quite a large project with many files and packages, users on the Free plan may not be able to compile it successfully on Overleaf. If that's the case, feel free to grab the PDF here, and download the sources as a .zip for offline perusal/compilation!
Erika Griechisch

Pico Presentation template
From https://egu2018.eu/PICO_how-to_guide_to_PICO.pdf
Abstracted and templated by Brian Ballsun-Stanton, Macquarie University.
Original template by https://github.com/snowtechblog/pico-latex-presentation by Anselm Köhler
Brian Ballsun-Stanton, Anselm Köhler

SOLAR SALES ON YOUR TRIP TO MARS
We study Logarithmically Spiral Trajectories and, in particular, we look for a solution to minimize the transit time of a Spacecraft propelled by a Solar Sail, while simultaneously minimizing the area of the Solar Sail, which would allow us to carry more payload on board. We start by analyzing the forces that act on the Spacecraft taking into account that its propellant is a Solar Sail; we use the studied forces to deduce the motion equations. We then solve this motion equation with a Runge-Kutta 4 method and transform the problem of minimizing time and area to a Non-linear Optimization problem. When solving the NLP we also try to minimize the relative final speed of th spacecraft with the destination planet in order to guarantee the possibility of a safe landing on its surface. The model improves when an angle parameter α (describing the angle formed by the Solar Sail with the colliding photons) is defined as a piecewise constant function and optimized whose values are optimized in every interval to minimize transit time and Area. Using the developed model to optimize the trajectory to be followed for sending from Earth to Mars a 2000kg-spacecraft propelled by a Solar Sail, subject to the condition that at trajectory start Mars and Earth were at their closest approach, and the Arrival Relative Velocity is less than 9km/s, give us a minimal transit time of 500days and a minimal area for the Solar Sail of 183158m2, meaning that the maximal payload would be 718kg. Compared with different number of partitions of α, the optimum stays stable. This gives a solid optimal trajectory and a great result for the numerical method used. Actually, waiting until the best moment to throw the Spacecraft, id est, Mars is at 1.14 radians respectively to Earth initial position, the minimal sail area 145950 m2 and, therefore, ables to transport until 978 kg of payload with the same transit time. In addition and to conclude we tried the model to optimize the inverse trajectory.
Marco Praderio Bova, Eneko Martin Martinez, & Maria dels Àngels Guinovart Llort