Master’s Degree in Aerospace Engineering School of Engineering – Forlì Campus University of Bologna Forlì, September 17 th 2019
Summary • Complete your enrolment times • Tuition fees and ER.GO • Forlì Campus services Scholarships • Upcoming events • Course units and study plan • Koinè association • Elective course units • Euroavia association • Teaching calendar and schedule • Contacts and websites • What to expect • International mobility • Language requirement • Facebook Page and group • Health and safety training • Aerospace student tutor • Facilities, services and opening
Welcome!
Complete your enrolment ALL THE STUDENTS must go to the Student Administration Office / Segreteria studenti of Forlì Padiglione Melandri Piazzale Solieri 1 47121 Forlì Go there with a valid ID document for the formal student identification and with the documents possibly indicated on the Call for applications at art.6. After that, the student career will be active and student badge/card can be collected. Non-identification will result in the impossibility to use services such as study plan submission, exam registration, WIFI access and library loan services.
Complete your enrolment Student badge self-service machines Badge self-service machines are available in specific points in the five Campuses: use the QR Code you received by email, you can print out your badge from any of the machines.
Complete your enrolment Particular situation or doubts, especially of Non-EU citizens with a VISA, can be discussed individually. Please send an email to cdlm.ae@unibo.it for an appointment. For all the information, please refer to the Student Handbook and Unibo website: http://www.unibo.it/en/teaching/enrolment-transfer-and-final-examination
Tuition fees and ER.GO Scholarships All students pay based on their Equivalent Financial Situation indicator (ISEE), irrespective of the degree programme that they enrol on . Full exemption is granted for ISEE values up to €23,000.00 . Above this threshold, the tuition fee increases proportionally to the ISEE value, with special subsidies for the lowest incomes. To pay a tuition fee calculated based on your economic situation, you must submit the application before October 30th 2019 by 18.00 (or by November 15th 2019 paying a 100 € fee). http://www.unibo.it/en/teaching/enrolment-transfer-and-final-examination/tuition-fees-and-exemptions/Tuition-fees/Tuition-fees International students should check at this link for the required documents: https://www.unibo.it/en/teaching/enrolment-transfer-and-final-examination/tuition-fees-and-exemptions/documentation-regarding- the-economic-situation-of-international-students
Tuition fees and ER.GO Scholarships ER.GO is the Regional Authority for the Right to Higher Education and it works very closely with the Universities to ensure that the needs of students are met. ER.GO provide University students with a variety of services, including financial assistance, residential accommodations, dining facilities, counseling and support, job and careers guidance Please check ER.GO Call for applications, deadlines and contact them for any questions: http://www.er-go.it/fileadmin/include/faq/index.php ER.GO staff is also available on Thursday afternoon from 14.30 to 16.00 at Forlì campus, P.le Solieri 1. ph. +39 0543 374810
Master’s degree in Aerospace Engineering programme website http://corsi.unibo.it/2cycle/AerospaceEngineering/Pages/default.aspx
Master’s Degree Programme content
Elective courses
Elective courses Elective courses selection, 1° year: 2 choices
Elective courses Elective courses selection, 2° year: 1 choice Students can also mix up elective course (Type D), but one Type B course from the Elective courses of guided choice must always be present in the study plan and must be taken in order to graduate. Students can also decide to pick up an extra Type D course.
Simulation and Modelling in Fluid Dynamics Elisabetta De Angelis Andrea Cimarelli Department of Industrial Engineering
Simulation and Modelling in Fluid Dynamics Numerical simulations Given the ever increasing performances of super computers, the numerical simulation in fluid dynamics is increasingly used for the design and development of engineering systems and for the prediction of natural phenomena.
Contents Discretization approaches Numerical techniques for the solution of the equations of fluid dynamics (Newton equation for continuum mechanics). Turbulence Multiscale phenomenon, many degrees of freedom. The Reynolds number of the applications cannot be handled by any super computer of the world by Direct Numerical Simulations. Modelling Aim to reduce the degrees of freedom of the problem. I ntroduction of models in the equations of fluid dynamics based on the current physical knowledge of turbulence.
Aims and structure of the course Aim of the course Providing basic knowledge for the analysis, simulation and modelling of turbulent flows. Topics Basics of numerical analysis. Discretization and solution techniques for the Navier-Stokes equations; Turbulence RANS, LES and DES models. Corseworks The students will be asked to carry out one of two assignments: 1- development of codes for the solution of the Navier-Stokes equations; 2- simulation of turbulent flows by means of CFD softwares.
Radio Communication and Radar Systems Master Degree in Aerospace Engineering Prof. Enrico Paolini Dept. of Electrical, Electronic, and Information Engineering “G. Marconi”
Why This Course? • Motivation : Space-to-Earth (air-to-Earth) or space-to-space (air-to-air) communication through electromagnetic waves is fundamental for flying objects such as aircrafts, spacecrafts, satellites, ISS, etc. Remote sensing capabilities of flying objects are also very important for monitoring, civil applications, defense. • Main objectives of the course: • To acquire knowledge about the main design criteria of wireless digital communication systems and the main metrics to evaluate their performance , such as bit error probability and spectral efficiency. • To acquire knowledge about the main approaches to tackle problems in radar systems .
Theoretical Foundation: Detection and Estimation Theory • Most problems in digital communication systems and in radar systems are decision- making or estimation problems which may be regarded as applications of detection and estimation theory . [ Decision-making ]: • Example What is the most likely transmitted symbol of information given a noisy observation of it? • Example [ Estimation problem ]: What are the carrier parameters (frequency, phase), given the noisy received radio-frequency signal? • Example [ Decision-making ]: Is an intruder present in some space (e.g., in some air space) given the noisy received wireless waveform? Example [ Estimation problem ] If the presence of an intruder has been detected, • what is its most likely position, given the received noisy signal and the past history? • For more information on the covered topics, please visit:
From Theory to Practice! • Several case studies considered during the lectures • Example: intruder detection with actual radar waveforms
Spacecraft Orbital Dynamics and Control (Marco Zannoni) Course Objectives Spacecraft Orbital Dynamics… • Understand the orbital dynamics of an artificial satellite, both in the case of motion around a planet or for interplanetary trajectories. … and Control • Understand the strategies for orbital maintenance, rendezvous, injection into an interplanetary trajectory and around a target planet.
Spacecraft Orbital Dynamics and Control (Marco Zannoni) Course topics Introduction to the Space Environment • Elements of Keplerian orbital mechanics • Gauss and Lagrange planetary equations • Effect of the main orbital perturbations • Station keeping maneuvers • Impulsive and continuous orbital transfers • Interplanetary Trajectories • Euler-Hill equations • Rendez-vous • Orbit Determination • Circular Restricted Three-Body Problem •
Spacecraft Orbital Dynamics and Control (Marco Zannoni) Hands on activities during the course Matlab exercises • Orbit determination and radio science data analysis of deep space • probes using NASA/JPL software NewIntegState( NewImpulseBurn( Body = ‘Cassini’, Body = 'PHX', Center = BodyName.Earth, Name = 'TCM1', InputFrame = CoordName.EME2000, Start = '13-AUG-2007 IntegFrame = CoordName.EME2000, ET', Mass = 0.000e+00 *kg, Frame = 'EME2000', State = [ DeltaMass = 0 *kg, 0.000e+00 *km, DeltaVel = [ 0.000e+00 *km, 2.22949E-03 *km/sec, 0.000e+00 *km, 1.06896E-02 *km/sec, 0.000e+00 *km/sec, 1.83506E-03 *km/sec, 0.000e+00 *km/sec, ], 0.000e+00 *km/sec, ) ], Forces = [ "Gravity", ], BeginTime = "01-JAN-2000 12:00:00 ET", EndTime = "01-JAN-2000 12:01:00 ET", EndEvents = [ ], )
Gunter’s space page Source: DLR Source: ESA SPACECRAFT SUBSYSTEMS SPACECRAFT SUBSYSTEMS AND SPACE MISSION DESIGN AND SPACE MISSION DESIGN Prem Sundaramoorthy Prem Sundaramoorthy
Why are some spacecraft so BIG ? And others so small ?
Why do some spacecraft look like this ?? And others like this ?
Can the phones we use everyday survive this Space environment?
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