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Total 21 records

    Experimental Investigation of the Effects of Canard Position on the Flowfield Over the Wing of a Model

    , M.Sc. Thesis Sharif University of Technology Izadkhah, Mohammad (Author) ; Soltani, Mohammad Reza (Supervisor)
    Abstract
    The analysis results of air combat simulations explain fighters succeed at close air combat that are super maneuverable and at high angle of attack controllable. Closed-coupled delta wing/canard configurations play an important role in modern aircraft design. These configurations offer high trimmed lift, improved agility and maneuverability as well, as a potential for increased lift-to drag ratio, all of which make them attractive to study. Experiments were carried out in a subsonic closed circuit wind tunnel over a delta wing model under the influence of canard. Canard was set in two different vertical positions, high and mid, with respect to the wing location. Flowfield measurements were... 

    Nonlinear Ship Maneuvering Simulation

    , M.Sc. Thesis Sharif University of Technology FathiKazerooni, Mohammadreza (Author) ; Seif, Mohammad Saeed (Supervisor)
    Abstract
    Ship maneuvering simulation and prediction in preliminary design stages has been concerned since forty years ago due to accidents occurred to large vessels and so many efforts have been held to develop the methods for simulation of ship maneuvering. Standards concerning ship maneuvering have been presented by International Maritime Organization that is known as a criteria to evaluate maneuvering performance of the ships. Traditionally ship maneuvering has been simulated in deep water and without any environmental conditions such as wind, wave, marine currents and effects resulted by asymmetric flow around ship hull during waterway entrance and shallow waters. Furthermore by introducing the... 

    Intelligent operation using terrain following flight in unmanned aerial vehicles

    , Article 2007 IEEE Aerospace Conference, Big Sky, MT, 3 March 2007 through 10 March 2007 ; 2007 ; 1095323X (ISSN) ; 1424405254 (ISBN); 9781424405251 (ISBN) Rahim, M ; Malaek, S. M. B ; Sharif University of Technology
    2007
    Abstract
    A novel approach in Terrain Following/Terrain Avoidance (TF/TA) flight is proposed. Due to existing unknown terrain during flight, an intelligent approach is used. Intelligence is implemented using the fuzzy approach. This method can be used in off-line design in trajectory planning which has wide applications in TF/TA maneuvers in unmanned aerial vehicles. A relationship between slope of terrain and aircraft height with speed of aircraft is constructed by fuzzy approach. This work is performed for a two dimensional Terrain Following Flight. This method is state of the art in literature. © 2007 IEEE  

    Collision avoidance maneuver for an autonomous vehicle

    , Article 9th IEEE International Workshop on Advanced Motion Control, 2006, Istanbul, 27 March 2006 through 29 March 2006 ; Volume 2006 , 2006 , Pages 249-254 Durali, M ; Amini Javid, G ; Kasaiezadeh, A ; Sharif University of Technology
    2006
    Abstract
    One of the most important capabilities expected from an autonomous vehicle is avoiding collision with obstacles in its path. For this purpose, autonomous vehicle must be able to perform an emergency maneuver as soon as the obstacle is detected. This paper presents a method for designing and performing an emergency maneuver in order to avoid collision with a fixed or moving obstacle in the path. A sinusoidal or exponential trajectory, which is a function of the relative distance between vehicle and obstacle, is designed as the desired trajectory for lateral motion of the vehicle. A sliding mode controller is designed in order to guarantee that the vehicle tracks that desired trajectory. The... 

    A neural network aided adaptive second-order gaussian filter for tracking maneuvering targets

    , Article ICTAI 2005: 17th IEEE International Conference on Tools with Artificial Intelligence, ICTAI'05, Hong Kong, 14 November 2005 through 16 November 2005 ; Volume 2005 , 2005 , Pages 439-446 ; 10823409 (ISSN); 0769524885 (ISBN); 9780769524887 (ISBN) Sadati, N ; Langary, D ; Sharif University of Technology
    2005
    Abstract
    The adaptive capability of filters is known to be increased by incorporating a neural network into the filtering procedure. In this paper, an adaptive algorithm for tracking maneuvering targets based on neural networks is proposed. This algorithm is implemented with two filters based on the current statistical model and a multilayer feedforward neural network. The two filters track the same maneuvering target in parallel and the neural network automatically considers all the state information of the two filters and adaptively adjusts the process variance of one of them to achieve better performance in different target maneuver tracking. Simulations results show that the proposed adaptive... 

    Semi-optimal co-ordinated manoeuvres for aircraft conflict resolution

    , Article Aeronautical Journal ; Volume 109, Issue 1097 , 2005 , Pages 313-323 ; 00019240 (ISSN) Parastari, J ; Malaek, M. B ; Sharif University of Technology
    Royal Aeronautical Society  2005
    Abstract
    In this manuscript, a new concept of 2D-semi-optimal-circular-3-arced-path manoeuvres with constant speed for multiple aircraft cooperative conflict resolution is presented. This type of manoeuvres is based on appropriate commands to heading, speed and manoeuvreing time. According to aircraft turning dynamics, each aircraft manoeuvre is composed of three tangent circular arcs. The optimality of manoeuvres is based on the minimisation of weighted sum of kinetic energy for aircraft two-legged manoeuvres. In comparison, aircraft with lower weight factors bear more responsibility to resolve the conflicts. The effectiveness of the proposed algorithm for real time conflict resolution is... 

    Modeling and analysis of AN ultra light slow flyer with variable shape control surfaces using shape memory alloy actuators

    , Article Proceedings of the 7th Biennial Conference on Engineering Systems Design and Analysis - 2004, Manchester, 19 July 2004 through 22 July 2004 ; Volume 2 , 2004 , Pages 153-162 ; 0791841731 (ISBN); 9780791841730 (ISBN) Alasty, A ; Alemohamad, S. H ; Khiabani, R. H ; Khalighi, Y ; Sharif University of Technology
    American Society of Mechanical Engineers  2004
    Abstract
    Applying flexible variable shape control surfaces (wing and elevator) structures is a way to increase efficiency and maneuverability of the planes, which is recently under research. In this paper, modeling of the flight of an unmanned ultra light plane is discussed. The modeling is done based on a real ultra light plane presented recently. To increase maneuverability of the plane, flexible variable shape structures are designed for the wing and the elevator. In design procedure, having an ultra light plane is considered. The elevator and the wing are used as control surfaces for longitudinal and lateral maneuvers respectively. Shape memory alloys (SMA) are used for reshaping the flexible... 

    Design and Dynamical Modelling and Control of a Micro-swimmer with High Maneuverability

    , M.Sc. Thesis Sharif University of Technology Esfandbod, Alireza (Author) ; Nejat, Hossein (Supervisor) ; Meghdari, Ali (Supervisor)
    Abstract
    Up to now many different mechanisms have been proposed for a swimming micro robot, but most of the previously designed micro robots are not able to perform three- dimensional maneuver and the motion of the proposed swimmers are limited along a straight line or in a plane. Some important issues that must be ruled in designing micro robots include: reduced number of actuators, high maneuverability, high motion controllability and elimination of lateral drift. In this study the aim is to design a micro swimmer with the aforementioned capabilities as much as possible. In this regard, many different ideas based on the quadrotor motion, flagellated bacteria and spiral flagellated bacteria, Fish... 

    Numerical analysis of wake structure and performance of two oscillatory mechanisms of a foil: Pure pitching and undulating

    , Article Proceedings of the Institution of Mechanical Engineers Part M: Journal of Engineering for the Maritime Environment ; Volume 229, Issue 4 , April , 2015 , Pages 376-396 ; 14750902 (ISSN) Abbaspoor, M ; Ebrahimi, M ; Sharif University of Technology
    SAGE Publications Ltd  2015
    Abstract
    There are various propulsion, maneuvering, and stabilization mechanisms in nature, which can provide inspiration for similar mechanisms in man-made vehicles. This study aims to elucidate and compare the propulsive vortical signature and performance of a foil in two important natural mechanisms of pure pitching and undulatory oscillations. Governing equations are solved with a pressure-based finite volume method solver, in an arbitrary Lagrangian-Eulerian framework domain containing a NACA 0012 foil moving with prescribed kinematics. The results show that in a given Reynolds number (Re), the undulating mechanism produces thrust at a higher Strouhal number (St) and with smaller growth slope,... 

    Modification of Design Target Area, based on Aircraft Terrain Following Missions

    , M.Sc. Thesis Sharif University of Technology Khosravi, Arash (Author) ; Malaek, Mohammad Bagher (Supervisor)
    Abstract
    This work investigates the possibility of developing suitable design guidelines for aircraft flying in very low altitude as well as terrain following flights (TFF). The work aims to highlight the TFF mission in the early stages of design process; as oppose to other mission conducted by the aircraft. Current approach in TFF relies heavily on efficient Flight Control System (FCS) regardless of the overall configuration of aircraft. However, in this work, we show not all aircraft in the service could conduct TFF and maneuverability of airplane is very important. In fact, we investigate the overall impact of TFF on the wing loading (W/S) and thrust loading (T/W); if we were to design an aircraft... 

    Design and Fabrication of a Swimmer Robot at Low Reynolds Number

    , Ph.D. Dissertation Sharif University of Technology Bahmanyar, Shahnaz (Author) ; Sayyadi, Hassan (Supervisor)
    Abstract
    Helical swimming robots with a capable propulsion system at low Reynolds numbers have been proposed for many applications. Although linear propulsion characteristics of swimming robots with a single helical flagellum have been extensively studied, the characteristics of maneuverability have not been completely investigated yet. In this thesis two novel mechanisms was proposed. The first mechanism presents a new method for the maneuverability of the helical swimming robot with a single helical flagellum. This mechanism is based on the change in the angle between the helical and body axes. This study shows that a change in the aforementioned angle can enable the swimming robot to have turning... 

    Design, Fabrication and Control of a Tilting-Rotor Quadrotor

    , M.Sc. Thesis Sharif University of Technology Bagheri, Alireza (Author) ; Nejat, Hossein (Supervisor) ; Behzadipour, Saeed (Supervisor)
    Abstract
    This project deals with the design, fabrication and control of a tilting-rotor quadrotor. This type of UAV can have high maneuverability in all 6 degrees of freedom (3D attitude and 3D position). The rotor axes can be tilted independently to produce desired force and torque vectors. This capability resolves limitations of the classic quadrotors and provides independent control of orientation and position. To control this UAV, we have proposed a control scheme relating the desired trajectory to the required forces and torques. Then a PID controller for the simultaneous control of position and attitude is designed. This controller is tested in a simulation and the results show that the control... 

    Comparative numerical analysis of the flow pattern and performance of a foil in flapping and undulating oscillations

    , Article Journal of Marine Science and Technology (Japan) ; Volume 20, Issue 2 , June , 2015 , Pages 257-277 ; 09484280 (ISSN) Abbaspour, M ; Ebrahimi, M ; Sharif University of Technology
    Springer-Verlag Tokyo  2015
    Abstract
    Nature presents a variety of propulsion, maneuvering, and stabilization mechanisms which can be inspired to design and construction of manmade vehicles and the devices involved in them, such as stabilizers or control surfaces. This study aims to elucidate and compare the propulsive vortical signature and performance of a foil in two important natural mechanisms: flapping and undulation. Navier–Stokes equations are solved in an ALE framework domain containing a 2D NACA 0012 foil moving with prescribed kinematics. All simulations are carried out using a pressure-based finite volume method solver. The results of time-averaged inline force versus Strouhal number (St) show that in a given... 

    Attitude determination improvement in accelerated motions for maneuvering underwater vehicles

    , Article Applied Ocean Research ; Volume 104 , November , 2020 Mirzaei, M ; Hosseini, I ; Makarem, H ; Sharif University of Technology
    Elsevier Ltd  2020
    Abstract
    Attitude determination for underwater vehicles in control and navigation applications has been always an important issue. MEMS-based accelerometer and gyroscope data can be usually used to determine the underwater vehicle attitude. However, the gyroscope sensors suffer from bias problem and the accelerometer data is not reliable in the presence of the external acceleration for the attitude determination. Therefore, data fusion for these two sensors is used to determine the attitude. But it should be noted that the common fusion algorithm does not perceive some special maneuvering accelerated motions and the use of accelerometer data causes a mistake in determining the Euler angles in these... 

    Enhancing the roll dynamics of an AUV by contra-rotating-propellers

    , Article Ships and Offshore Structures ; Volume 16, Issue 7 , 2021 , Pages 787-796 ; 17445302 (ISSN) Ebrahimi, M ; Kamali, A ; Abbaspour, M ; Sharif University of Technology
    Taylor and Francis Ltd  2021
    Abstract
    Roll control of the Autonomous Underwater Vehicles (AUVs) is a significant issue in the current field of research for many researchers in the subject of AUV control system designation. Especially at higher speeds, the roll angle generated by a single rotating propeller or other external disturbances can considerably influence the whole dynamics and therefore the operation of the vehicle. In this paper, the utilisation of a system of contra-rotating-propellers (CRP) to enhance the roll dynamics of an AUV is evaluated by developing a six-degrees-of-freedom (6DOF) dynamics and control systems’ simulator. The results show that: 1. The single propeller system can cause roll angle deflections... 

    Variable structure controller design for steer-by-wire system of a passenger car

    , Article Journal of Mechanical Science and Technology ; Vol. 28, issue. 8 , Aug , 2014 , p. 3285-3299 Mousavinejad, I ; Kazemi, R ; Sharif University of Technology
    Abstract
    The electric power steering (EPS) system was developed and the steer-by-wire (SBW) system achieves the purposes of EPS. The advantages of SBW are packaging flexibility, advanced vehicle control system, and superior performance. No mechanical linkage exists between the steering gear and steering column in the SBW system. The steering wheel and front-wheel steering can be controlled independently. The SBW system consists of two motors controlled by an electronic control unit (ECU). One motor is in the steering wheel and develops the steering feel of the driver and the other motor is in the steering linkage and improves vehicle maneuverability and stability. Moreover, the active front steering... 

    A comparative numerical study on the performances and vortical patterns of two bioinspired oscillatory mechanisms: Undulating and pure heaving

    , Article Applied Bionics and Biomechanics ; Volume 2015 , 2015 ; 11762322 (ISSN) Ebrahimi, M ; Abbaspour, M ; Sharif University of Technology
    IOS Press  2015
    Abstract
    The hydrodynamics and energetics of bioinspired oscillating mechanisms have received significant attentions by engineers and biologists to develop the underwater and air vehicles. Undulating and pure heaving (or plunging) motions are two significant mechanisms which are utilized in nature to provide propulsive, maneuvering, and stabilization forces.This study aims to elucidate and compare the propulsive vortical signature and performance of these two important natural mechanisms through a systematic numerical study. Navier-Stokes equations are solved, by a pressure-based finite volume method solver, in an arbitrary Lagrangian- Eulerian (ALE) framework domain containing a 2D NACA0012 foil... 

    Integrated guidance and control of elastic flight vehicle based on robust MPC

    , Article International Journal of Robust and Nonlinear Control ; Volume 25, Issue 15 , 2015 , Pages 2608-2630 ; 10498923 (ISSN) Shamaghdari, S ; Nikravesh, S. K. Y ; Haeri, M ; Sharif University of Technology
    John Wiley and Sons Ltd  2015
    Abstract
    Integrated guidance and control of an elastic flight vehicle based on constrained robust model predictive control is proposed. The design is based on a partial state feedback control law that minimizes a cost function within the framework of linear matrix inequalities. It is shown that the solution of the defined optimization problem stabilizes the nonlinear plant. Nonlinear kinematics and dynamics are taken into account, and internal stability of the closed-loop nonlinear system is guaranteed. The performance and effectiveness of the proposed integrated guidance and control against non-maneuvering and weaving targets are evaluated using computer simulations  

    Enhancing the roll dynamics of an AUV by contra-rotating-propellers

    , Article Ships and Offshore Structures ; 2020 Ebrahimi, M ; Kamali, A ; Abbaspour, M ; Sharif University of Technology
    Taylor and Francis Ltd  2020
    Abstract
    Roll control of the Autonomous Underwater Vehicles (AUVs) is a significant issue in the current field of research for many researchers in the subject of AUV control system designation. Especially at higher speeds, the roll angle generated by a single rotating propeller or other external disturbances can considerably influence the whole dynamics and therefore the operation of the vehicle. In this paper, the utilisation of a system of contra-rotating-propellers (CRP) to enhance the roll dynamics of an AUV is evaluated by developing a six-degrees-of-freedom (6DOF) dynamics and control systems’ simulator. The results show that: 1. The single propeller system can cause roll angle deflections... 

    Multiple model extended continuous ant colony filter applied to real-time wind estimation in a fixed-wing UAV

    , Article Engineering Applications of Artificial Intelligence ; Volume 92 , 2020 Nobahari, H ; Sharifi, A ; Sharif University of Technology
    Elsevier Ltd  2020
    Abstract
    In this study, a new heuristic multiple model filter, called Multiple Model Extended Continuous Ant Colony Filter, is proposed to solve a nonlinear multiple model state estimation problem. In this filter, a bank of extended continuous ant colony filters are run in parallel to solve the multiple model estimation problem. The probability of each model is continually updated and consequently both the true model and the states of the nonlinear system are updated based on the weighted sum of the filters. The new multiple model filter is tested on an engineering problem. The problem is to estimate simultaneously the states of a fixed-wing unmanned aerial vehicle as well as the wind model, applied...