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    Non linear predictive model control of batch polymerization of methyl methacrylate for thernal trajectory tracking

    , Article Amirkabir (Journal of Science and Technology) ; Volume 14, Issue 55 C , 2003 , Pages 811-824 ; 10150951 (ISSN) Rafizadeh, M ; Abbaszadeh, M ; Sharif University of Technology
    2003
    Abstract
    A nonlinear predictive model controller was designed to control the temperature of a batch polymerization of methyl methacrylate. Using the mechanistic model of the polymerization, a state space model was derived and converted to transfer function model. The coefficients of the transfer function were calculated along the selected temperature trajectory by sequential linearization. 140 operation points were resulted. Model validation showed model ability in process dynamic description. Consequently, DMC algorithm was applied and one objective function was optimized. Results of control loop simulation shows a high precision ability of this algorithm in comparison to classic methods  

    Estimation of the Price Elasticity of Gasoline Smuggling Demand in Iran

    , M.Sc. Thesis Sharif University of Technology Rafizadeh, Nima (Author) ; Rahmati, Mohammad Hossein (Supervisor)
    Abstract
    This study investigates the price elasticity of gasoline smuggling demand in Iran. For this purpose, a panel data of monthly gasoline consumption has been used that contains data for 160 regions of distribution for Iran's Oil Production Company between 2005 and 2014. The results of estimating the monthly elasticity of gasoline smuggling demand in each region show a significant impact of the gasoline price differential between Iran and its neighboring countries, as well as the distance of each region with the neighboring countries on the demand. The results of this study show that whenever gasoline prices increase inside the country, the inclination to smuggling has been decreased due to a... 

    The effects of intermediate and post-annealing phenomena on the mechanical properties and microstructure of constrained groove pressed copper sheet

    , Article Materials Science and Engineering A ; Volume 515, Issue 1-2 , 2009 , Pages 162-168 ; 09215093 (ISSN) Rafizadeh, E ; Mani, A ; Kazeminezhad, M ; Sharif University of Technology
    2009
    Abstract
    Commercial purity copper sheets were subjected to a severe plastic deformation technique known as constrained groove pressing (CGP). The effect of pass number, intermediate and post-annealing on the yield strength, hardness and final microstructure of the copper specimens were investigated. The initial pass increases the strength much more than the subsequent passes. Intermediate and post-annealing up to 300 °C cannot change the mechanical properties significantly and even in some cases improve the strength and hardness while reduce the hardness inhomogeneity. Microstructure after post-annealing at elevated temperatures shows abnormal grain growth. © 2009 Elsevier B.V. All rights reserved  

    Constrained model predictive control of MMA polymerization reactor based on genetic algorithm optimization

    , Article Proceedings of 2003 IEEE Conference on Control Applications, Istanbul, 23 June 2003 through 25 June 2003 ; Volume 1 , 2003 , Pages 464-469 Rafizadeh, M ; Solgi, R ; Abbaszadeh, M ; Sharif University of Technology
    2003
    Abstract
    Control of MMA polymerization batch reactor has intensively investigated. The nonlinear and time varying behavior of the system makes its control a challenging task. MPC algorithm is enjoying an increasing application for control of chemical processes. A sequential linearized model based predictive controller based on the DMC algorithm was designed to control the temperature of a batch MMA polymerization reactor. A genetic algorithm (GA) is suggested to optimize the cost function of DMC. The controller performance was studied via simulation. The controller performance in tracking the profile, noise and disturbances rejection is very good  

    Machine learning in energy economics and finance: A review

    , Article Energy Economics ; Volume 81 , 2019 , Pages 709-727 ; 01409883 (ISSN) Ghoddusi, H ; Creamer, G. G ; Rafizadeh, N ; Sharif University of Technology
    Elsevier B.V  2019
    Abstract
    Machine learning (ML) is generating new opportunities for innovative research in energy economics and finance. We critically review the burgeoning literature dedicated to Energy Economics/Finance applications of ML. Our review identifies applications in areas such as predicting energy prices (e.g. crude oil, natural gas, and power), demand forecasting, risk management, trading strategies, data processing, and analyzing macro/energy trends. We critically review the content (methods and findings) of more than 130 articles published between 2005 and 2018. Our analysis suggests that Support Vector Machine (SVM), Artificial Neural Network (ANN), and Genetic Algorithms (GAs) are among the most... 

    On the evolution of flow stress during constrained groove pressing of pure copper sheet

    , Article Computational Materials Science ; Volume 45, Issue 4 , 2009 , Pages 855-859 ; 09270256 (ISSN) Hosseini, E ; Kazeminezhad, M ; Mani, A ; Rafizadeh, E ; Sharif University of Technology
    2009
    Abstract
    Using a mechanical model and dislocation density based model, the evolutions of dislocation density and flow stress of pure copper during constrained groove pressing (CGP) process are investigated. In this regard, the strain and strain rate are achieved from the mechanical model and then input into the dislocation model. To verify the predicted flow stress, the process of constrained groove pressing is performed on the sheets of pure copper from one to three passes. The predicted flow stresses are compared with the experimental data and a good agreement is observed. Also, it is found that during the straining of the copper sheet in CGP process, the dislocation density and strength dropping... 

    Characterization of Ceramic Coating Synthesized on Magnesium Alloy Substrate by Plasma Electrolytic Oxidation Process

    , M.Sc. Thesis Sharif University of Technology Rafizadeh, Ehsan (Author) ; Faghihi Sani, Mohammad Ali (Supervisor)
    Abstract
    Plasma electrolytic oxidation (PEO) is currently recognized as an effective coating method on active metals such as magnesium. In this method, through occurrence of strong electric discharges on the surface of the anode accompanied by electrochemical and thermo-chemical reactions at plasma environment, a relatively thick ceramic coating with complex compounds grows on the metal surface which significantly improves its properties. Regarding the influence of PEO electrical parameters on the morphology and other properties of the coating, the objective of the present study is to prepare a quality ceramic coating on AZ31 magnesium alloy substrate via setting the process parameters, such as... 

    Effect of current frequency on coating properties formed on aluminised steel by plasma electrolytic oxidation

    , Article Surface Engineering ; Vol. 30, issue. 3 , 2014 , pp. 224-228 ; ISSN: 02670844 Jafarniya Kharanagh, V ; Faghihi Sani, M. A ; Rafizadeh, E ; Sharif University of Technology
    2014
    Abstract
    In the present study, plasma electrolytic oxidation process was carried out on aluminised steel with a pulsed bipolar electrical source at different frequencies, namely, 50, 300, 600 and 1500 Hz with constant 50% duty cycle for 10 min in an alkaline silicate electrolyte. Morphology, wear behaviour and corrosion resistance of the coatings were investigated by scanning electron microscopy, pin on disc and potentiodynamic polarisation experiment in 3·5 wt-%NaCl solution. The results showed that with increasing the pulse frequency, the density of the residual pores increases, but their size as well as the coating thickness decreases. The corrosion current density of the coating processed at 1500... 

    Control of a 5-Link Parallel Robot with Computational Intelligent Techniques

    , M.Sc. Thesis Sharif University of Technology Rafizadeh, Roya (Author) ; Seifipour, Navid (Supervisor) ; Jahed, Mehran (Co-Advisor)
    Abstract
    Control of parallel robots continues to be a challenging research topic. The structural variety of such robots dictated by the application and function makes such control strategies even more unique. As these robots often require nonlinear control schemes, such research has been focused towards two general controlling computational intelligent methods, namely adaptive (and optimal) control and artificial intelligence (e.g. fuzzy and Neural Net) based control. This study considers Neural Net (NNs) and fuzzy control method in order to propose a control scheme for a newly introduced 5-link parallel robot which has 3 degrees of freedom operating in a single plane environment (i.e. two... 

    Fabrication and Characterization of a UF Ceramic Membrane based on TiO_2 Nanoparticles

    , M.Sc. Thesis Sharif University of Technology Mirkazemi, Amin (Author) ; Taghavinia, Nima (Supervisor)
    Abstract
    UF membranes are widely used in various industries now, a major type of these membranes are ceramic membranes which are resistant to high temperatures and corrosive fluids. In this thesis we developed an anisotropic UF ceramic membrane based on 20nm TiO2 nanoparticles on a prous sustrate. We had two major challenges, the first one was to find a suitable prous substrate and the second one was to find an appropriate coating method. Our main task was to optimise the process conditions to achive a crackless and uniform membrane layer with minimal ups and downs. Lots of coating methods and TiO2 inks have been tried, finally we used a coating method which we called it “Soft Blade Coating”, with... 

    Continuous-thrust Trajectory Optimization in the Binary Asteroids System

    , M.Sc. Thesis Sharif University of Technology Ashrafi, Mehnraz (Author) ; Asadian, Nima (Supervisor)
    Abstract
    In this thesis, the optimal trajectories of a spacecraft in the binary asteroids system is studied. The objective functions of optimal trajectories in these system are the maximum coverage of the asteroids surface and minimum time and fuel consumption. For this purpose, the dynamic of binary system is modeled. The binary system of 1999 KW4 is selected as a case study. The ellipsoid-sphere model is a good approximation for the case of this study. In this model, the asteroids orbit in a circular orbit around each other in a spin-spin-orbit resonance configuration, in which the asteroids’ rotational velocity is equal to orbital mean motion. Then, the equations of motion of the spacecraft as the... 

    Fabrication and Characterization of Inverted Perovskite Solar Cells Using Nickel Oxide as Hole Transporting Layer

    , Ph.D. Dissertation Sharif University of Technology Saki, Zahra (Author) ; Taghavinia, Nima (Supervisor)
    Abstract
    In this research, we study and optimize the inverted perovskite solar cells (PSCs) using nano layers of NiOx and Li:NiOx as hole transporting layers (HTLs) and nano layers of PC70BM and C60 as electron transporting layers (ETLs). We fabricated inverted PSCs with three different HTLs, namely MoOx, PEDOT:PSS and NiOx, using vapor assisted solution processed (VASP) method for making MAPbI3 perovskite which yielded a power conversion efficiency (PCE) of 1%, 1.93% and 3.65%, respectively. Solution-processed deposition method, high transparency (˃90%) and high band gap (3.9 eV) are the most advantages to use NiOx as HTL in current research. Using lithium as dopant to the NiOx increases the... 

    Coupled Rotational and Translational Modelling of Two Satellite Tethered Formation and their Robust Attitude Control

    , M.Sc. Thesis Sharif University of Technology Darabi, Atefe (Author) ; Assadian, Nima (Supervisor)
    Abstract
    The 6DOF modelling and robust attitude control of two tethered satellites using tether tension moments is studied in this thesis. In this regard, the coupled rotational and translational dynamics of two satellites connected by a tether in the presence of Earth’s gravitational perturbation, aerodynamic drag, solar radiation pressure and third body effects (Sun and Moon) and also uncertainties in some of physical parameters of system and sensor’s outputs is modelled. Moreover, the tether attachment point to the satellites is different from their center of mass and its effect on dynamics of the system is taken into consideration. Then, the attitude of both satellites are controlled using robust... 

    Fault Tolerant Model Predictive Control of Tethered Satellite System

    , M.Sc. Thesis Sharif University of Technology Ramezani, Mahya (Author) ; Asadian, Nima (Supervisor)
    Abstract
    In this thesis, a control method to cope with the fault in the two-satellite two-tether satellite systems has been proposed to avoid failing the mission in the case one tether is torn. A new model for the tethered satellite system with two tethers has been developed to show the effects of tethers’ tension forces in the attitude dynamics. One of the main features of this model is the ability of changing the tethers’ connection points to the co-satellite for attitude control purposes. As a result, tethers’ tension forces are used as control actions to reduce the fuel consumption. The introduced coupled tethered satellite system has been controlled using the model predictive control method.... 

    Fault-Tolerant Attitude Control of Satellite with Thrusters Using μ-synthesis

    , M.Sc. Thesis Sharif University of Technology Taheri, Abdolreza (Author) ; Assadian, Nima (Supervisor)
    Abstract
    In this project, a fault-tolerant attitude control system is developed for thruster-driven satellites. The proposed method has the advantage over current state-of-the-art approaches in that it does not require a fault detection and isolation system. Generalized moments are generated by a robust controller that is designed using mixed sensitivity H_∞ and μ-synthesis by DK-iteration. Moreover, a pulse-width modulation technique with quadratic programming optimization is tuned to map the controller outputs to thruster on-off commands as efficiently as possible. The controller is designed to tolerate up to ±30% perturbations in inertia properties and thrust degradations up to 90% of the nominal... 

    Integrated Control and Estimation of Satellite Attitude using Adaptive Nero-Fuzzy Inference System

    , M.Sc. Thesis Sharif University of Technology Abtahi, Mehdi (Author) ; Assadian, Nima (Supervisor)
    Abstract
    This paper presents an integrated attitude control and estimation of satellite by using adaptive neural fuzzy (ANFIS) logic, indeed a system which using ANFIS controller and estimator is considered then an ANFIS simulator that can control and estimate contemporary is supposed. ANFIS system has been trained by using data obtained from an optimal PID controller. Then ANFIS controller performance has been compared with the performance of a PID controller, the analogy has repeated in different situations such as noise and uncertainty. Results show that system with ANFIS controller is more optimal than PID’s in all these situations. After that ANFIS estimator is studied and results indicate the... 

    Dynamics of Tethered Satellite Formation Around Binary Asteroids

    , M.Sc. Thesis Sharif University of Technology Bakhshipour, Mehran (Author) ; Assadian, Nima (Supervisor)
    Abstract
    Studying of binary asteroids because of achieving data of existence sources in the world persuades to investigate about tethered satellite formation around binary asteroids in future missions. About 20 percent of asteroids around the sun are binary asteroids. It is going to analyse dynamics of tethered satellite around Didymos binary asteroid. Light mass of the asteroid is good reason to consider gravitational harmonic perturbation, and leads to attention about solar radiation pressure depends on distance in modelling of the dynamical system. It will be zonal harmonics up to second order and sectoral. Satellites are such a particle as an assumption; that is why attitude motion of satellites... 

    Fractional Order Modeling and Control of Flexible Satellite

    , M.Sc. Thesis Sharif University of Technology Hosseini, Masoud (Author) ; Assadian, Nima (Supervisor)
    Abstract
    In recent decades the structure of space systems has gained more complexity due to the development of space technology. Usage of larger structure in spacecraft could cause undesirable structural vibration. mNeglecting this phenomena would affect the performance of satellite subsystems specially the accuracy of satellite control subsystem. By implementing fractional order calculus in modeling of flexible satellite, the damping effect could be modeled better than classical damping model. Also using fractional order integrator and differentiator operator will increase the performance of control subsystem. In this research, the fractional order calculus has been used in modeling and control of... 

    Spacecraft Rendezvous and Docking Using Adaptive Neuro-Fuzzy Inference System

    , M.Sc. Thesis Sharif University of Technology Tallebi, Morteza (Author) ; Asadian, Nima (Supervisor)
    Abstract
    In this research an ANFIS controller will be developed to rendezvous and dock with a non-cooperative spacecraft; the controller must make the spacecraft reach the velocity and nearby position of the target spacecraft. Due to uncertainty in modeling and changes in the moment inertia tensor, the controller must be able to adapt with these changes and uncertainty, these changes may happen because of robotic arm or solar panel movings. Robustness of the controller will be evaluated by applying orbital disturbances and modeling errors through monte-carlo simulations. To model the spacecraft the specifications of a known spacecraft will be used but some specifications may be studied parametricaly.... 

    Attitude and Deformation Estimation of Flexible Satellite Using Magnetometer and Sun Sensor

    , M.Sc. Thesis Sharif University of Technology Ghani, Marzieh (Author) ; Asadian, Nima (Supervisor)
    Abstract
    The estimation of attitude and deformation of a flexible satellite using magnetometer and sun sensor data are studied in this thesis. To this end, the dynamical differential equations of the flexible satellite have been derived using Lagrange’s equation. These equations of motion are then utilized for the purpose of simulation and verification. After introducing the measurements equations, the observability of the satellite with flexible panels has been evaluated. Afterward, the attitude of the satellite body and deformation of the flexible panels have been estimated by EKF (Extended Kalman Filter) as well as UKF (Unscented Kalman Filter). The results show that the estimations using UKF are...