Integration of robotic inverse kinematic routines in an algorithmic 3D modeling software

An industrial manipulator equipped with an automatic clay extruder is used to realize a machine that can manufacture additively clay objects. The desired geometries are designed by means of a 3D modeling software and then sliced in a sequence of layers with the same thickness of the extruded clay section. The profiles of each layer are transformed in trajectories for the extruder and therefore for the end-effector of the manipulator. The goal of this thesis is to improve the algorithm for the inverse kinematic resolution and the integration of the routine within the development software that controls the machine (Rhino/Grasshopper). The kinematic model is described by homogeneous transformations, adopting the Denavit-Hartenberg standard convention. The function is implemented in C# and it has been preliminarily tested in Matlab. The outcome of this work is a substantial reduction of the computation time relative to the execution of the algorithm, which is halved.

Energy harvesting from piezoelectric devices embedded in a 3D printed wing

This thesis work has been carried out at Clarkson University in Potsdam NY, USA and involved the design of a low elongation wing, consisting of parts made by polylactide (PLA) using the fused deposition model (FDM) technology of Rapid Prototyping, then assembled together in a thin aluminum spar. The aim of the research is to evaluate the feasibility of collecting electrical energy by converting mechanical energy from the vibration of the wing flutter. With this aim piezoelectric stripes were glued in the inner part of the wing, as well as on the aluminum spar, as monomorphic configuration. During the phases of the project, particular attention was given to the geometry and the materials used, in order to trigger the flutter for low flow velocity. The CAD software SolidWorks® was used for the design of the wing and then the drawings were sent to the Clarkson machine shop in order to to produce the parts required by the wing assembly. FEM simulations were performed, using software MSC NASTRAN/PATRAN®, to evaluate the stiffness of the whole wing as well as the natural vibration modes of the structure. These data, in a first approximation, were used to predict the flutter speed. Finally, experimental tests in the Clarkson wind tunnel facility were carried out in order to validate the results obtained from FEM analysis. The power collected by the piezoelectrics under flutter condition was addressed by tuning the resistors downstream the electronic circuit of the piezoelectrics.

AGV Safety Areas Obstacle Detection and Interaction with Point Cloud Derived Map

This thesis project aims to the development of an algorithm for the obstacle detection and the interaction between the safety areas of an Automated Guided Vehicles (AGV) and a Point Cloud derived map inside the context of a CAD software. The first part of the project focuses on the implementation of an algorithm for the clipping of general polygons, with which has been possible to: construct the safety areas polygon, derive the sweep of this areas along the navigation path performing a union and detect the intersections with line or polygon representing the obstacles. The second part is about the construction of a map in terms of geometric entities (lines and polygons) starting from a point cloud given by the 3D scan of the environment. The point cloud is processed using: filters, clustering algorithms and concave/convex hull derived algorithms in order to extract line and polygon entities representing obstacles. Finally, the last part aims to use the a priori knowledge of possible obstacle detections on a given segment, to predict the behavior of the AGV and use this prediction to optimize the choice of the vehicle's assigned velocity in that segment, minimizing the travel time.

Progetto e modellazione CAD di parti per comandi di simulatore di volo di elicottero da produrre con tecniche additive

La tesi di laurea, di tipo sperimentale, nasce dall’esigenza di progettare un sistema di force feedback da installare sui comandi di un simulatore di volo per elicottero, prevedendo di utilizzare tecnologie additive per la produzione dei componenti. Sono state, quindi, presentate alcune proposte per il soddisfacimento dei requisiti di progetto. Tra le due soluzioni progettuali individuate, una è stata scartata, mentre l'altra, basata su un collare da montare sul comando del ciclico e su un disegno per il supporto del sistema di ritenuta, è stata sviluppata. Sono state fatte, di conseguenza, assieme a quelle di tipo progettuale, alcune scelte legate alla pianificazione meccanica (ad esempio, scelta delle viti e delle molle). Il risultato finale è un sistema di force feedback funzionante, in cui la leva del comando ciclico del simulatore di volo per elicottero oppone uno sforzo in seguito ad una deflessione da parte del pilota.

Studio sulla vulnerabiltà sismica della clinica neurologica di Bologna

In questo studio di tesi è stata eseguita un' analisi storico critica sugli edifici del complesso della Clinica Neurologica di Bologna, sono state valutate le sollecitazioni attraverso una modellazione 3D con software agli elementi finiti SAP2000, e sono state eseguite le verifiche dei meccanismi di collasso globali, locali ed inoltre verifiche di deformabiltà.

La strategia BIM a supporto del progetto della sicurezza nel cantiere edile: il caso dell'ospedale di primo soccorso a Lampedusa.

Throughout this research, the whole life cycle of a building will be analyzed, with a special focus on the most common issues that affect the construction sector nowadays, such as safety. In fact, the goal is to enhance the management of the entire construction process in order to reduce the risk of accidents. The contemporary trend is that of researching new tools capable of reducing, or even eliminating, the most common mistakes that usually lead to safety risks. That is one of the main reasons why new technologies and tools have been introduced in the field. The one we will focus on is the so-called BIM: Building Information Modeling. With the term BIM we refer to wider and more complex analysis tool than a simple 3D modeling software. Through BIM technologies we are able to generate a multi-dimension 3D model which contains all the information about the project. This innovative approach aims at a better understanding and control of the project by taking into consideration the entire life cycle and resulting in a faster and more sustainable way of management. Furthermore, BIM software allows for the sharing of all the information among the different aspects of the project and among the different participants involved thus improving the cooperation and communication. In addition, BIM software utilizes smart tools that simulate and visualize the process in advance, thus preventing issues that might not have been taking into consideration during the design process. This leads to higher chances of avoiding risks, delays and cost increases. Using a hospital case study, we will apply this approach for the completion of a safety plan, with a special focus onto the construction phase.

Design methods and geometric modelling of scaffolds for bone tissue engineering

Every year, thousand of surgical treatments are performed in order to fix up or completely substitute, where possible, organs or tissues affected by degenerative diseases. Patients with these kind of illnesses stay long times waiting for a donor that could replace, in a short time, the damaged organ or the tissue. The lack of biological alternates, related to conventional surgical treatments as autografts, allografts, e xenografts, led the researchers belonging to different areas to collaborate to find out innovative solutions. This research brought to a new discipline able to merge molecular biology, biomaterial, engineering, biomechanics and, recently, design and architecture knowledges. This discipline is named Tissue Engineering (TE) and it represents a step forward towards the substitutive or regenerative medicine. One of the major challenge of the TE is to design and develop, using a biomimetic approach, an artificial 3D anatomy scaffold, suitable for cells adhesion that are able to proliferate and differentiate themselves as consequence of the biological and biophysical stimulus offered by the specific tissue to be replaced. Nowadays, powerful instruments allow to perform analysis day by day more accurateand defined on patients that need more precise diagnosis and treatments.Starting from patient specific information provided by TC (Computed Tomography) microCT and MRI(Magnetic Resonance Imaging), an image-based approach can be performed in order to reconstruct the site to be replaced. With the aid of the recent Additive Manufacturing techniques that allow to print tridimensional objects with sub millimetric precision, it is now possible to practice an almost complete control of the parametrical characteristics of the scaffold: this is the way to achieve a correct cellular regeneration. In this work, we focalize the attention on a branch of TE known as Bone TE, whose the bone is main subject. Bone TE combines osteoconductive and morphological aspects of the scaffold, whose main properties are pore diameter, structure porosity and interconnectivity. The realization of the ideal values of these parameters represents the main goal of this work: here we'll a create simple and interactive biomimetic design process based on 3D CAD modeling and generative algorithmsthat provide a way to control the main properties and to create a structure morphologically similar to the cancellous bone. Two different typologies of scaffold will be compared: the first is based on Triply Periodic MinimalSurface (T.P.M.S.) whose basic crystalline geometries are nowadays used for Bone TE scaffolding; the second is based on using Voronoi's diagrams and they are more often used in the design of decorations and jewellery for their capacity to decompose and tasselate a volumetric space using an heterogeneous spatial distribution (often frequent in nature). In this work, we will show how to manipulate the main properties (pore diameter, structure porosity and interconnectivity) of the design TE oriented scaffolding using the implementation of generative algorithms: "bringing back the nature to the nature".

Leap Aided Modelling (LAM) in Blender

L'evoluzione tecnologica e l'utilizzo crescente della computer grafica in diversi settori stanno suscitando l'interesse di sempre più persone verso il mondo della modellazione 3D. I software di modellazione, tuttavia, si presentano spesso inadeguati all'utilizzo da parte di utenti senza esperienza, soprattutto a causa dei comandi di navigazione e modellazione poco intuitivi. Dal punto di vista dell'interazione uomo-computer, questi software devono infatti affrontare un grande ostacolo: il rapporto tra dispositivi di input 2D (come il mouse) e la manipolazione di una scena 3D. Il progetto presentato in questa tesi è un addon per Blender che consente di utilizzare il dispositivo Leap Motion come ausilio alla modellazione di superfici in computer grafica. L'obiettivo di questa tesi è stato quello di progettare e realizzare un'interfaccia user-friendly tra Leap e Blender, in modo da potere utilizzare i sensori del primo per facilitare ed estendere i comandi di navigazione e modellazione del secondo. L'addon realizzato per Blender implementa il concetto di LAM (Leap Aided Modelling: modellazione assistita da Leap), consentendo quindi di estendere le feature di Blender riguardanti la selezione, lo spostamento e la modifica degli oggetti in scena, la manipolazione della vista utente e la modellazione di curve e superfici Non Uniform Rational B-Splines (NURBS). Queste estensioni sono state create per rendere più veloci e semplici le operazioni altrimenti guidate esclusivamente da mouse e tastiera.

Numerical Analysis and Redesign of a High Speed Linear Cascade Wind Tunnel for Aircraft Gas Turbine Engines Testing

Linear cascade testing serves a fundamental role in the research, development, and design of turbomachines as it is a simple yet very effective way to compute the performance of a generic blade geometry. These kinds of experiments are usually carried out in specialized wind tunnel facilities. This thesis deals with the numerical characterization and subsequent partial redesign of the S-1/C Continuous High Speed Wind Tunnel of the Von Karman Institute for Fluid Dynamics. The current facility is powered by a 13-stage axial compressor that is not powerful enough to balance the energy loss experienced when testing low turning airfoils. In order to address this issue a performance assessment of the wind tunnel was performed under several flow regimes via numerical simulations. After that, a redesign proposal aimed at reducing the pressure loss was investigated. This consists of a linear cascade of turning blades to be placed downstream of the test section and designed specifically for the type of linear cascade being tested. An automatic design procedure was created taking as input parameters those measured at the outlet of the cascade. The parametrization method employed Bézier curves to produce an airfoil geometry that could be imported into a CAD software so that a cascade could be designed. The proposal was simulated via CFD analysis and proved to be effective in reducing pressure losses up to 41%. The same tool developed in this thesis could be adopted to design similar apparatuses and could also be optimized and specialized for the design of turbomachines components.

Conceptualization of an Electric Compact SUV for the American and Italian Market using the IDeS Method

Electric cars are increasingly popular due to a transition of mobility towards more sustainable forms. From an increasingly green and pollution reduction perspective, there are more and more incentives that encourage customers to invest in electric cars. Using the Industrial Design and Structure (IDeS) research method, this project has the aim to design a new electric compact SUV suitable for all people who live in the city, and for people who move outside urban areas. In order to achieve the goal of developing a new car in the industrial automotive environment, the compact SUV segment was chosen because it is a vehicle very requested by the costumers and it is successful in the market due to its versatility. IDeS is a combination of innovative and advanced systematic approaches used to set up a new industrial project. The IDeS methodology is sequentially composed of Quality Function Deployment (QFD), Benchmarking (BM), Top-Flop analysis (TFA), Stylistic Design Engineering (SDE), Design for X, Prototyping, Testing, Budgeting, and Planning. The work is based on a series of steps and the sequence of these must be meticulously scheduled, imposing deadlines along the work. Starting from an analysis of the market and competitors, the study of the best and worst existing parameters in the competitor’s market is done, arriving at the idea of a better product in terms of numbers and innovation. After identifying the characteristics that the new car should have, the other step is the styling part, with the definition of the style and the design of the machine on a 3D CAD. Finally, it switches to the prototyping and testing phase to see if the product is able to work. Ultimately, intending to place the car on the market, it is essential to estimate the necessary budget for a possible investment in this project.

Modellazione grafica di elicotteri per la simulazione del volo

L'obiettivo di questo elaborato di tesi è la modellazione grafica delle cabine di pilotaggio di due elicotteri civili: si prevede una futura implementazione del modello di volo completo sul simulatore FlightGear. I due velivoli presi in considerazione sono stati sviluppati dall'azienda AgustaWestland e sono denominati AW109 e AW139. I modelli di volo sono composti da una parte grafica e dal modello dinamico del volo. La presente tesi si occupa del primo aspetto. Il lavoro di tesi è iniziato con una fase preliminare di ricerca che ha richiesto lo studio di come i modelli dinamici di volo siano implementati nel simulatore FlightGear; è stato, inoltre, approfondito l'utilizzo del linguaggio di markup XML necessario a descrivere il funzionamento e le caratteristiche dei velivoli in FlightGear. Ha fatto seguito la fase di scrittura dei file XML, facendo riferimento a modelli di elicotteri preesistenti e all'effettiva modellazione degli strumenti di bordo, attraverso il programma CAD Blender. Nella fase finale sono stati studiati e posizionati i vari strumenti principali di bordo, consultando i manuali degli elicotteri e ottenendo delle cabine di pilotaggio del tutto simili a quelle reali dei velivoli considerati. Gli sviluppi futuri di questo lavoro prevedono l'integrazione dei modelli grafici qui implementati nel modello di volo completo dei due elicotteri presi in considerazione.

A new concept for a Sport-Coupè car developed with the Industrial Design Structure method (IDeS)

The aim of this study, conducted in collaboration with Lawrence Technological University in Detroit, is to create, through the method of the Industrial Design Structure (IDeS), a new concept for a sport-coupe car, based on a restyling of a retro model (Ford Mustang 1967). To date, vintage models of cars always arouse great interest both for the history behind them and for the classic and elegant style. Designing a model of a vehicle that can combine the charm of retro style with the innovation and comfort of modern cars would allow to meet the needs and desires of a large segment of the market that today is forced to choose between past and future. Thanks to a well-conceived concept car an automaker company is able to express its future policy, to make a statement of intent as, such a prototype, ticks all the boxes, from glamour and visual wow-factor to technical intrigue and design fascination. IDeS is an approach that makes use of many engineering tools to realize a study developed on several steps that must be meticulously organized and timed. With a deep analysis of the trends dominating the automotive industry it is possible to identify a series of product requirements using quality function deployment (QFD). The considerations from this first evaluation led to the definition of the technical specifications via benchmarking (BM) and top-flop analysis (TFA). Then, the structured methodology of stylistic design engineering (SDE) is applied through six phases: (1) stylistic trends analysis; (2) sketches; (3) 2D CAD drawings; (4) 3D CAD models; (5) virtual prototyping; (6) solid stylistic model. Finally, Developing the IDeS method up to the final stages of Prototypes and Testing you get a product as close as possible to the ideal vehicle conceptualized in the initial analysis.

Un applicativo Web con tecnologia single-page AJAX, servizi REST e grafica X3D, per la configurazione di modelli CAD tridimensionali

In questa tesi è stato realizzato un sistema web-based, per la configurazione di modelli meccanici tridimensionali. L’intero software è basato su architettura multi-tier. Il back-end espone servizi RESTful che permettono l’interrogazione di una base di dati contenente l’anagrafica dei modelli e l’interazione con il CAD 3D SolidWorks. Il front-end è rappresentato da due pagine HTML ideate come SPA (Single Page Application), una per l’amministratore e l’altra per l’utente finale; esse sono responsabili delle chiamate asincrone verso i servizi, dell’aggiornamento automatico dell’interfaccia e dell’interazione con immagini tridimensionali.

Progetto preliminare e modellazione CAD di dirigibile per riprese aeree

Scopo del presente lavoro di tesi è dimensionare a livello preliminare e modellare con software CAD 3D, un dirigibile non-rigido per riprese aeree di eventi sportivi o musicali. Il dimensionamento viene svolto attraverso un metodo tratto dalla bibliografia che si avvale di un processo iterativo che cerca la convergenza tra il peso ottenuto in base al carburante necessario per la missione da compiere e il peso ottenuto sommando tutti i contributi dei componenti del dirigibile, al variare del volume dell’involucro. La descrizione del metodo è preceduta da un’introduzione che descrive alcuni concetti fondamentali legati alle innovazioni che si sono susseguite nel tempo a livello di progettazione e dimensionamento strutturale dei dirigibili. Il dimensionamento ottenuto dal processo iterativo è stato preso come base per la modellazione CAD di un dirigibile equipaggiato con un sistema composto da una camera per riprese aeree e batterie per permettere l'alimentazione degli apparati video e di trasmissione.

Studio e analisi di software per il porting di codice a 64 bit

XCModel è un sistema CAD, basato su NURBS, realizzato ed utilizzato in ambiente accademico. È composto da quattro pacchetti per la modellazione 2D, 3D e la resa foto-realistica, ognuno dotato di una propria interfaccia grafica. Questi pacchetti sono in costante evoluzione: sia per le continua evoluzioni dell’hardware che ai cambiamenti degli standard software. Il sistema nel complesso raccoglie la conoscenza e l’esperienza nella modellazione geometrica acquisita nel tempo dai progettisti. XCModel, insieme ai suoi sottosistemi, sono stati progettati per diventare un laboratorio di insegnamento e ricerca utile a sperimentare ed imparare metodi ed algoritmi nella modellazione geometrica e nella visualizzazione grafica. La natura principalmente accademica, e la conseguente funzione divulgativa, hanno richiesto continui aggiornamenti del programma affinché potesse continuare a svolgere la propria funzione nel corso degli anni. La necessità di continuare a ad evolversi, come software didattico, anche con il moderno hardware, è forse il principale motivo della scelta di convertire XCModel a 64 bit; una conversione che ho svolto in questa tesi. Come molte altre applicazioni realizzate a 32 bit, la maggior parte del codice viene eseguito correttamente senza problemi. Vi sono però una serie di problematiche, a volte molto subdole, che emergono durante la migrazione delle applicazioni in generale e di XCModel in particolare. Questa tesi illustra i principali problemi di portabilità riscontrati durante il porting a 64 bit di questo pacchetto seguendo il percorso da me intrapreso: mostrerò gli approcci adottati, i tool utilizzati e gli errori riscontrati.