In-Flight Collision Avoidance Controller Based Only on OS4 Embedded Sensors

The major goal of this research was the development and implementation of a control system able to avoid collisions during the flight for a mini-quadrotor helicopter, based only on its embedded sensors without changing the environment. However, it is important to highlight that the design aspects must be seriously considered in order to overcome hardware limitations and achieve control simplification. The controllers of a UAV (Unmanned Aerial Vehicle) robot deal with highly unstable dynamics and strong axes coupling. Furthermore, any additional embedded sensor increases the robot total weight and therefore, decreases its operating time. The best balance between embedded electronics and robot operating time is desired. This paper focuses not only on the development and implementation of a collision avoidance controller for a mini-robotic helicopter using only its embedded sensors, but also on the mathematical model that was essential for the controller developing phases. Based on this model we carried out the development of a simulation tool based on MatLab/Simulink that was fundamental for setting the controllers' parameters. This tool allowed us to simulate and improve the OS4 controllers in different modeled environments and test different approaches. After that, the controllers were embedded in the real robot and the results proved to be very robust and feasible. In addition to this, the controller has the advantage of being compatible with future path planners that we are developing.

Speed Neuro-fuzzy Estimator Applied To Sensorless Induction Motor Control

This work proposes the development of an Adaptive Neuro-fuzzy Inference System (ANFIS) estimator applied to speed control in a three-phase induction motor sensorless drive. Usually, ANFIS is used to replace the traditional PI controller in induction motor drives. The evaluation of the estimation capability of the ANFIS in a sensorless drive is one of the contributions of this work. The ANFIS speed estimator is validated in a magnetizing flux oriented control scheme, consisting in one more contribution. As an open-loop estimator, it is applied to moderate performance drives and it is not the proposal of this work to solve the low and zero speed estimation problems. Simulations to evaluate the performance of the estimator considering the vector drive system were done from the Matlab/Simulink(R) software. To determine the benefits of the proposed model, a practical system was implemented using a voltage source inverter (VSI) to drive the motor and the vector control including the ANFIS estimator, which is carried out by the Real Time Toolbox from Matlab/Simulink(R) software and a data acquisition card from National Instruments.

A control and automation system for wave basins

This paper presents the new active absorption wave basin, named Hydrodynamic Calibrator (HC), constructed at the University of São Paulo (USP), in the Laboratory facilities of the Numerical Offshore Tank (TPN). The square (14 m 14 m) tank is able to generate and absorb waves from 0.5 Hz to 2.0 Hz, by means of 148 active hinged flap wave makers. An independent mechanical system drives each flap by means of a 1HP servo-motor and a ball-screw based transmission system. A customized ultrasonic wave probe is installed in each flap, and is responsible for measuring wave elevation in the flap. A complex automation architecture was implemented, with three Programmable Logic Computers (PLCs), and a low-level software is responsible for all the interlocks and maintenance functions of the tank. Furthermore, all the control algorithms for the generation and absorption are implemented using higher level software (MATLAB /Simulink block diagrams). These algorithms calculate the motions of the wave makers both to generate and absorb the required wave field by taking into account the layout of the flaps and the limits of wave generation. The experimental transfer function that relates the flap amplitude to the wave elevation amplitude is used for the calculation of the motion of each flap. This paper describes the main features of the tank, followed by a detailed presentation of the whole automation system. It includes the measuring devices, signal conditioning, PLC and network architecture, real-time and synchronizing software and motor control loop. Finally, a validation of the whole automation system is presented, by means of the experimental analysis of the transfer function of the waves generated and the calculation of all the delays introduced by the automation system.

Modellazione multibody di veicoli ferroviari: sviluppo ed implementazione di modelli innovativi per l'analisi del contatto ruota - rotaia

The wheel - rail contact analysis plays a fundamental role in the multibody modeling of railway vehicles. A good contact model must provide an accurate description of the global contact phenomena (contact forces and torques, number and position of the contact points) and of the local contact phenomena (position and shape of the contact patch, stresses and displacements). The model has also to assure high numerical efficiency (in order to be implemented directly online within multibody models) and a good compatibility with commercial multibody software (Simpack Rail, Adams Rail). The wheel - rail contact problem has been discussed by several authors and many models can be found in the literature. The contact models can be subdivided into two different categories: the global models and the local (or differential) models. Currently, as regards the global models, the main approaches to the problem are the so - called rigid contact formulation and the semi – elastic contact description. The rigid approach considers the wheel and the rail as rigid bodies. The contact is imposed by means of constraint equations and the contact points are detected during the dynamic simulation by solving the nonlinear algebraic differential equations associated to the constrained multibody system. Indentation between the bodies is not permitted and the normal contact forces are calculated through the Lagrange multipliers. Finally the Hertz’s and the Kalker’s theories allow to evaluate the shape of the contact patch and the tangential forces respectively. Also the semi - elastic approach considers the wheel and the rail as rigid bodies. However in this case no kinematic constraints are imposed and the indentation between the bodies is permitted. The contact points are detected by means of approximated procedures (based on look - up tables and simplifying hypotheses on the problem geometry). The normal contact forces are calculated as a function of the indentation while, as in the rigid approach, the Hertz’s and the Kalker’s theories allow to evaluate the shape of the contact patch and the tangential forces. Both the described multibody approaches are computationally very efficient but their generality and accuracy turn out to be often insufficient because the physical hypotheses behind these theories are too restrictive and, in many circumstances, unverified. In order to obtain a complete description of the contact phenomena, local (or differential) contact models are needed. In other words wheel and rail have to be considered elastic bodies governed by the Navier’s equations and the contact has to be described by suitable analytical contact conditions. The contact between elastic bodies has been widely studied in literature both in the general case and in the rolling case. Many procedures based on variational inequalities, FEM techniques and convex optimization have been developed. This kind of approach assures high generality and accuracy but still needs very large computational costs and memory consumption. Due to the high computational load and memory consumption, referring to the current state of the art, the integration between multibody and differential modeling is almost absent in literature especially in the railway field. However this integration is very important because only the differential modeling allows an accurate analysis of the contact problem (in terms of contact forces and torques, position and shape of the contact patch, stresses and displacements) while the multibody modeling is the standard in the study of the railway dynamics. In this thesis some innovative wheel – rail contact models developed during the Ph. D. activity will be described. Concerning the global models, two new models belonging to the semi – elastic approach will be presented; the models satisfy the following specifics: 1) the models have to be 3D and to consider all the six relative degrees of freedom between wheel and rail 2) the models have to consider generic railway tracks and generic wheel and rail profiles 3) the models have to assure a general and accurate handling of the multiple contact without simplifying hypotheses on the problem geometry; in particular the models have to evaluate the number and the position of the contact points and, for each point, the contact forces and torques 4) the models have to be implementable directly online within the multibody models without look - up tables 5) the models have to assure computation times comparable with those of commercial multibody software (Simpack Rail, Adams Rail) and compatible with RT and HIL applications 6) the models have to be compatible with commercial multibody software (Simpack Rail, Adams Rail). The most innovative aspect of the new global contact models regards the detection of the contact points. In particular both the models aim to reduce the algebraic problem dimension by means of suitable analytical techniques. This kind of reduction allows to obtain an high numerical efficiency that makes possible the online implementation of the new procedure and the achievement of performance comparable with those of commercial multibody software. At the same time the analytical approach assures high accuracy and generality. Concerning the local (or differential) contact models, one new model satisfying the following specifics will be presented: 1) the model has to be 3D and to consider all the six relative degrees of freedom between wheel and rail 2) the model has to consider generic railway tracks and generic wheel and rail profiles 3) the model has to assure a general and accurate handling of the multiple contact without simplifying hypotheses on the problem geometry; in particular the model has to able to calculate both the global contact variables (contact forces and torques) and the local contact variables (position and shape of the contact patch, stresses and displacements) 4) the model has to be implementable directly online within the multibody models 5) the model has to assure high numerical efficiency and a reduced memory consumption in order to achieve a good integration between multibody and differential modeling (the base for the local contact models) 6) the model has to be compatible with commercial multibody software (Simpack Rail, Adams Rail). In this case the most innovative aspects of the new local contact model regard the contact modeling (by means of suitable analytical conditions) and the implementation of the numerical algorithms needed to solve the discrete problem arising from the discretization of the original continuum problem. Moreover, during the development of the local model, the achievement of a good compromise between accuracy and efficiency turned out to be very important to obtain a good integration between multibody and differential modeling. At this point the contact models has been inserted within a 3D multibody model of a railway vehicle to obtain a complete model of the wagon. The railway vehicle chosen as benchmark is the Manchester Wagon the physical and geometrical characteristics of which are easily available in the literature. The model of the whole railway vehicle (multibody model and contact model) has been implemented in the Matlab/Simulink environment. The multibody model has been implemented in SimMechanics, a Matlab toolbox specifically designed for multibody dynamics, while, as regards the contact models, the CS – functions have been used; this particular Matlab architecture allows to efficiently connect the Matlab/Simulink and the C/C++ environment. The 3D multibody model of the same vehicle (this time equipped with a standard contact model based on the semi - elastic approach) has been then implemented also in Simpack Rail, a commercial multibody software for railway vehicles widely tested and validated. Finally numerical simulations of the vehicle dynamics have been carried out on many different railway tracks with the aim of evaluating the performances of the whole model. The comparison between the results obtained by the Matlab/ Simulink model and those obtained by the Simpack Rail model has allowed an accurate and reliable validation of the new contact models. In conclusion to this brief introduction to my Ph. D. thesis, we would like to thank Trenitalia and the Regione Toscana for the support provided during all the Ph. D. activity. Moreover we would also like to thank the INTEC GmbH, the society the develops the software Simpack Rail, with which we are currently working together to develop innovative toolboxes specifically designed for the wheel rail contact analysis.

Sviluppo di modelli motore e veicolo per l'analisi di strategie di controllo in applicazioni Software e Hardware In the Loop

This work describes the development of a simulation tool which allows the simulation of the Internal Combustion Engine (ICE), the transmission and the vehicle dynamics. It is a control oriented simulation tool, designed in order to perform both off-line (Software In the Loop) and on-line (Hardware In the Loop) simulation. In the first case the simulation tool can be used in order to optimize Engine Control Unit strategies (as far as regard, for example, the fuel consumption or the performance of the engine), while in the second case it can be used in order to test the control system. In recent years the use of HIL simulations has proved to be very useful in developing and testing of control systems. Hardware In the Loop simulation is a technology where the actual vehicles, engines or other components are replaced by a real time simulation, based on a mathematical model and running in a real time processor. The processor reads ECU (Engine Control Unit) output signals which would normally feed the actuators and, by using mathematical models, provides the signals which would be produced by the actual sensors. The simulation tool, fully designed within Simulink, includes the possibility to simulate the only engine, the transmission and vehicle dynamics and the engine along with the vehicle and transmission dynamics, allowing in this case to evaluate the performance and the operating conditions of the Internal Combustion Engine, once it is installed on a given vehicle. Furthermore the simulation tool includes different level of complexity, since it is possible to use, for example, either a zero-dimensional or a one-dimensional model of the intake system (in this case only for off-line application, because of the higher computational effort). Given these preliminary remarks, an important goal of this work is the development of a simulation environment that can be easily adapted to different engine types (single- or multi-cylinder, four-stroke or two-stroke, diesel or gasoline) and transmission architecture without reprogramming. Also, the same simulation tool can be rapidly configured both for off-line and real-time application. The Matlab-Simulink environment has been adopted to achieve such objectives, since its graphical programming interface allows building flexible and reconfigurable models, and real-time simulation is possible with standard, off-the-shelf software and hardware platforms (such as dSPACE systems).

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

Comparative Analysis of Alternative Hybrid Systems for Automotive Applications

The main objective of this work was to investigate the impact of different hybridization concepts and levels of hybridization on fuel economy of a standard road vehicle where both conventional and non-conventional hybrid architectures are treated exactly in the same way from the point of view of overall energy flow optimization. Hybrid component models were developed and presented in detail as well as the simulations results mainly for NEDC cycle. The analysis was performed on four different parallel hybrid powertrain concepts: Hybrid Electric Vehicle (HEV), High Speed Flywheel Hybrid Vehicle (HSF-HV), Hydraulic Hybrid Vehicle (HHV) and Pneumatic Hybrid Vehicle (PHV). In order to perform equitable analysis of different hybrid systems, comparison was performed also on the basis of the same usable system energy storage capacity (i.e. 625kJ for HEV, HSF and the HHV) but in the case of pneumatic hybrid systems maximal storage capacity was limited by the size of the systems in order to comply with the packaging requirements of the vehicle. The simulations were performed within the IAV Gmbh - VeLoDyn software simulator based on Matlab / Simulink software package. Advanced cycle independent control strategy (ECMS) was implemented into the hybrid supervisory control unit in order to solve power management problem for all hybrid powertrain solutions. In order to maintain State of Charge within desired boundaries during different cycles and to facilitate easy implementation and recalibration of the control strategy for very different hybrid systems, Charge Sustaining Algorithm was added into the ECMS framework. Also, a Variable Shift Pattern VSP-ECMS algorithm was proposed as an extension of ECMS capabilities so as to include gear selection into the determination of minimal (energy) cost function of the hybrid system. Further, cycle-based energetic analysis was performed in all the simulated cases, and the results have been reported in the corresponding chapters.

Design and implementation of a novel multi-constellation FPGA-based dual frequency GNSS receiver for space applications

The PhD activity described in the document is part of the Microsatellite and Microsystem Laboratory of the II Faculty of Engineering, University of Bologna. The main objective is the design and development of a GNSS receiver for the orbit determination of microsatellites in low earth orbit. The development starts from the electronic design and goes up to the implementation of the navigation algorithms, covering all the aspects that are involved in this type of applications. The use of GPS receivers for orbit determination is a consolidated application used in many space missions, but the development of the new GNSS system within few years, such as the European Galileo, the Chinese COMPASS and the Russian modernized GLONASS, proposes new challenges and offers new opportunities to increase the orbit determination performances. The evaluation of improvements coming from the new systems together with the implementation of a receiver that is compatible with at least one of the new systems, are the main activities of the PhD. The activities can be divided in three section: receiver requirements definition and prototype implementation, design and analysis of the GNSS signal tracking algorithms, and design and analysis of the navigation algorithms. The receiver prototype is based on a Virtex FPGA by Xilinx, and includes a PowerPC processor. The architecture follows the software defined radio paradigm, so most of signal processing is performed in software while only what is strictly necessary is done in hardware. The tracking algorithms are implemented as a combination of Phase Locked Loop and Frequency Locked Loop for the carrier, and Delay Locked Loop with variable bandwidth for the code. The navigation algorithm is based on the extended Kalman filter and includes an accurate LEO orbit model.

Grid Connected Doubly Fed Induction Generator Based Wind Turbine under LVRT

This project concentrates on the Low Voltage Ride Through (LVRT) capability of Doubly Fed Induction Generator (DFIG) wind turbine. The main attention in the project is, therefore, drawn to the control of the DFIG wind turbine and of its power converter and to the ability to protect itself without disconnection during grid faults. It provides also an overview on the interaction between variable speed DFIG wind turbines and the power system subjected to disturbances, such as short circuit faults. The dynamic model of DFIG wind turbine includes models for both mechanical components as well as for all electrical components, controllers and for the protection device of DFIG necessary during grid faults. The viewpoint of this project is to carry out different simulations to provide insight and understanding of the grid fault impact on both DFIG wind turbines and on the power system itself. The dynamic behavior of DFIG wind turbines during grid faults is simulated and assessed by using a transmission power system generic model developed and delivered by Transmission System Operator in the power system simulation toolbox Digsilent, Matlab/Simulink and PLECS.

Studio e implementazione di un autopilota su un UAV ad ala fissa

Si riporta inizialmente un’analisi tecnica dell’autopilota Ardupilot, utilizzato con il firmware Arduplane, che predispone la scheda all’utilizzo specifico su velivoli senza pilota ad ala fissa. La parte sostanziale della tesi riguarda invece lo studio delle leggi di controllo implementate su Arduplane e la loro modellazione, assieme ad altre parti del codice, in ambiente Matlab Simulink. Il sistema di controllo creato, chiamato Attitude Flight System, viene verificato con la tecnica del Software In the Loop in un simulatore di volo virtuale modellato anch’esso in Simulink, si utilizza la dinamica di un velivolo UAV di prova e il software FlightGear per l’ambiente grafico. Di fondamentale importanza è la verifica della compatibilità fra il firmware originale e il codice generato a partire dai modelli Simulink, verifica effettuata mediante test di tipo Hardware in the Loop. L’ultima parte della tesi descrive le prove di volo svolte per verificare le prestazioni della scheda su un aeromodello trainer.

Sviluppo e implementazione di un sistema di biofeedback per il controllo del sodio plasmatico in emodialisi

L’obiettivo della tesi è stato quello di integrare un feedback sul sodio plasmatico all’interno di un sistema di biofeedback sul volume ematico già esistente. I vantaggi del nuovo sistema risiedono nella capacità del sistema di rispondere in modo ancora più accurato alle specifiche esigenze dei singoli pazienti. Il sistema è stato implementato in Matlab/Simulink. Sono stati effettuate 72 simulazioni di trattamenti reali di emodialisi. Il sistema si è dimostrato capace di portare a compimento il raggiungimento dei target di sodio plasmatico e volume ematico, con rimozione delle masse di sodio dal plasma simile a quella ottenuta utilizzando il sistema privo di feedback sul sodio plasmatico.

Teoria del consenso e applicazione al problema del coordinamento del moto di robot.

Il sempre crescente numero di applicazioni di reti di sensori, robot cooperanti e formazioni di veicoli, ha fatto sì che le problematiche legate al coordinamento di sistemi multi-agente (MAS) diventassero tra le più studiate nell’ambito della teoria dei controlli. Esistono numerosi approcci per affrontare il problema, spesso profondamente diversi tra loro. La strategia studiata in questa tesi è basata sulla Teoria del Consenso, che ha una natura distribuita e completamente leader-less; inoltre il contenuto informativo scambiato tra gli agenti è ridotto al minimo. I primi 3 capitoli introducono ed analizzano le leggi di interazione (Protocolli di Consenso) che permettono di coordinare un Network di sistemi dinamici. Nel capitolo 4 si pensa all'applicazione della teoria al problema del "loitering" circolare di più robot volanti attorno ad un obiettivo in movimento. Si sviluppa a tale scopo una simulazione in ambiente Matlab/Simulink, che genera le traiettorie di riferimento di raggio e centro impostabili, a partire da qualunque posizione iniziale degli agenti. Tale simulazione è stata utilizzata presso il “Center for Research on Complex Automated Systems” (CASY-DEI Università di Bologna) per implementare il loitering di una rete di quadrirotori "CrazyFlie". I risultati ed il setup di laboratorio sono riportati nel capitolo 5. Sviluppi futuri si concentreranno su algoritmi locali che permettano agli agenti di evitare collisioni durante i transitori: il controllo di collision-avoidance dovrà essere completamente indipendente da quello di consenso, per non snaturare il protocollo di Consenso stesso.

Modellistica e determinazione della dinamica di un quadrotor UAV per fini di controllo

Nella tesi vengono proposte una modellazione di un quadrotor affetto da un campo vettoriale incognito aerodinamico e la sua identificazione basata su non linear geometric approach e su reti neurali a funzione di base radiale (RBF). Il non linear geometric approach viene utilizzato per il disaccoppiamento delle componenti incognite aerodinamiche mentre le modellazione RBF dei coefficienti permette di applicare un algoritmo ai minimi quadrati per l'identificazione del sistema. Infine viene implementato un simulatore in ambiente MATLAB Simulink per la validazione della metodologia. Le simulazioni effettuate dimostrano la bontà del metodo proposto.

Sviluppo di un tool per lo studio di configurazioni architetturali nell'ambito di un simulatore orbitale e di assetto per microsatelliti

La realizzazione della componentistica satellitare è una disciplina innovativa e sempre in aggiornamento, capitanata dall’obiettivo di minimizzare il peso e il volume delle componenti e concretizzare così missioni satellitari affidabili ma sempre più economiche. Questo lavoro di tesi viene svolto nell’ambito di strumenti per la simulazione di sistemi di controllo di assetto di un satellite in orbita bassa terrestre. Il lavoro è volto ad ottenere uno strumento per compiere studi preliminari di missioni di microsatelliti, che sia dotato della possibilità di scegliere più combinazioni di attuatori e sensori e che permetta di valutare la bontà e i vantaggi derivanti dalla scelta di tali configurazioni scelte. Il punto di partenza è stato un simulatore realizzato in ambiente Matlab/Simulink per il monitoraggio di uno specifico microsatellite, ALMASat-1 dell’Università di Bologna. Vi sono stati aggiunti dei tools allo scopo di aggiornare il simulatore a nuove tecnologie e di consentire di realizzare diverse combinazioni di determinazione e controllo in assetto. Si presenterà inizialmente l’interfaccia grafica realizzata per facilitare l’utilizzo del simulatore e si mostreranno successivamente le modifiche apportate in concomitanza con l’aggiornamento del simulatore. Tra le innovazioni applicate al simulatore si annoverano la possibilità di far iniziare la simulazione in precisi stadi di assetto, permettendo all’utente di discriminare solo le fasi ad egli utili, e il miglioramento del sistema di determinazione dell’assetto, compiuto aggiungendo al sistema un simulatore di sensore di stelle, il più accurato tra tutti i sensori e il cui utilizzo, tipicamente riservato a missioni ad elevato budget, si è reso recentemente compatibile, in termini di dimensioni peso e costi, anche a piattaforme satellitari di dimensioni ridotte. Per entrambi gli aspetti verranno mostrate le rispettive modalità di realizzazione, ponendo particolare attenzione all’analisi posta per l’implementazione di uno strumento di misura. Infine sarà presente una discussione sui vantaggi offerti dal simulatore rinnovato.

Modellazione elettromeccanica di una macchina automatica opercolatrice

Nella tesi si è studiata una macchina automatica per l'industria farmaceutica: l'Adapta 100, un'opercolatrice (macchina riempi-capsule) prodotta da IMA SpA. Gli scopi della tesi erano chiarire il flusso di potenza dei vari assi e valutare un possibile risparmio energetico. La macchina infatti ha diversi motori: uno, collegato all'asse master, che comanda i gruppi non rimovibili e gli altri che comandano i gruppi di dosaggio. Tali motori in generale, per qualche tratto del ciclo della macchina, potranno lavorare come generatori, anche considerando il solo funzionamento a regime: si avrà cioè, in qualche istante, che le forze esterne tendono ad accelerare il motore, che così assorbe energia meccanica e produce energia elettrica. Attualmente tale energia viene dissipata in apposite resistenze collegate ai motori; ci si è chiesti se non si potesse invece immagazzinare l'energia prodotta, ad esempio per usarla in caso di black-out, per frenare delicatamente la macchina senza che gli assi perdano la fase. Un'alternativa è quella di ridistribuire la potenza generata istante per istante collegando i motori a un comune bus DC. Prima però è necessario conoscere gli andamenti di coppia e velocità di ciascun motore: per questo ci si è ricondotti al modello della macchina a 1 gdl, riducendo tutte le coppie e le inerzie all'asse motore. Si sono studiati i due assi più importanti in termini di coppie e potenze di picco: questi sono l'asse master e l'asse di dosaggio della polvere farmaceutica. Il modello è stato concretamente implementato con degli script MATLAB. Il modello risulta flessibile, per considerare le varie modalità di funzionamento della macchina, e considera i principali termini di coppia, inclusi attriti (inseriti sotto forma di rendimenti) e forze esterne di lavorazione. Tra queste è particolarmente importante la forza di compattazione della polvere, che è stata modellata con la formula di Kawakita, nota dalla letteratura.