Sviluppo e validazione sperimentale di strategie di previsione e controllo del fenomeno della preaccensione (Mega-Knock)

L’algoritmo per la previsione del Mega-Knock si inserisce all’interno di uno dei temi cardine dell’attuale ricerca nel campo motoristico: la minimizzazione del consumo di combustibile nei motori ad alto grado di sovralimentazione, sviluppati nell’ottica del downsizing. La possibilità di prevedere l’innescarsi del Mega-Knock consente di ottimizzare la definizione dell’obiettivo di titolo, evitando arricchimenti non necessari in un range di funzionamento del motore che frequentemente viene esplorato nella normale guida su strada. Si tratterà la possibilità di utilizzare una relazione empirica per cercare di arrivare alla previsione dell’insorgere della preaccensione, per poi ricorrere ad opportune strategie motore per evitare il verificarsi del fenomeno; il tutto tramite lo sviluppo di un algoritmo in ambiente MatLab-Simulink

ROP Gadgets hiding techniques in Open Source Projects

Today there are many techniques that allows to exploit vulnerabilities of an application; there are also many techniques that are designed to stop these exploit attacks. This thesis wants to highlight how a specific type of attack, based on a technique called Return Oriented Programming (ROP), can be easily applied to binaries with particular characteristics. A new method that allows the injection of "useful" code in an Open Source projects without arousing suspicions is presented; this is possible because of the harmless aspects of the injected code. This useful code facilitate a ROP attack against an executable that contains vulnerable bugs. The injection process can be visualized in environment where an user can contribute with own code to a particular Open Source project. This thesis also highlights how current software protections are not correctly applied to Open Source project, thus enabling the proposed approach.

Evolution of the structural and fracture design of the ISS payloads due to the new launchers, specifically applied to Biolab IEC-2 projects

The relatively young discipline of astronautics represents one of the scientifically most fascinating and technologically advanced achievements of our time. The human exploration in space does not offer only extraordinary research possibilities but also demands high requirements from man and technology. The space environment provides a lot of attractive experimental tools towards the understanding of fundamental mechanism in natural sciences. It has been shown that especially reduced gravity and elevated radiation, two distinctive factors in space, influence the behavior of biological systems significantly. For this reason one of the key objectives on board of an earth orbiting laboratory is the research in the field of life sciences, covering the broad range from botany, human physiology and crew health up to biotechnology. The Columbus Module is the only European low gravity platform that allows researchers to perform ambitious experiments in a continuous time frame up to several months. Biolab is part of the initial outfitting of the Columbus Laboratory; it is a multi-user facility supporting research in the field of biology, e.g. effect of microgravity and space radiation on cell cultures, micro-organisms, small plants and small invertebrates. The Biolab IEC are projects designed to work in the automatic part of Biolab. In this moment in the TO-53 department of Airbus Defence & Space (formerly Astrium) there are two experiments that are in phase C/D of the development and they are the subject of this thesis: CELLRAD and CYTOSKELETON. They will be launched in soft configuration, that means packed inside a block of foam that has the task to reduce the launch loads on the payload. Until 10 years ago the payloads which were launched in soft configuration were supposed to be structural safe by themselves and a specific structural analysis could be waived on them; with the opening of the launchers market to private companies (that are not under the direct control of the international space agencies), the requirements on the verifications of payloads are changed and they have become much more conservative. In 2012 a new random environment has been introduced due to the new Space-X launch specification that results to be particularly challenging for the soft launched payloads. The last ESA specification requires to perform structural analysis on the payload for combined loads (random vibration, quasi-steady acceleration and pressure). The aim of this thesis is to create FEM models able to reproduce the launch configuration and to verify that all the margins of safety are positive and to show how they change because of the new Space-X random environment. In case the results are negative, improved design solution are implemented. Based on the FEM result a study of the joins has been carried out and, when needed, a crack growth analysis has been performed.

Controlli non distruttivi su mega-coaster: risultati sperimentali e azioni correttive

Il lavoro di tesi è focalizzato sull'utilizzo dei controlli non distruttivi (NDT) nell'ambito della manutenzione industriale, in particolare al controllo di un mega-coaster. Dopo una breve panoramica sulle tecniche di indagine più utilizzate, si prosegue nell'ambito specifico dei controlli eseguiti all'interno del parco divertimenti di Mirabilandia, sull'attrazione di punta, ovvero l'inverted-coaster "KATUN". In particolare viene descritto il controllo del tracciato dell'attrazione, ovvero del binario, mediante tecnica ad ultrasuoni. L'elaborato si conclude con un riassunto dei risultati sperimentali ottenuti ed alcune azioni correttive intraprese per il miglioramento dell'efficacia dei controlli stessi.