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Total 258 records

    Near-optimal terrain collision avoidance trajectories using elevation maps

    , Article 2006 IEEE Aerospace Conference, Big Sky, MT, 4 March 2006 through 11 March 2006 ; Volume 2006 , 2006 ; 1095323X (ISSN); 0780395468 (ISBN); 9780780395466 (ISBN) Malaek, M. B ; Abbasi, A ; Sharif University of Technology
    2006
    Abstract
    The main attempt of this paper is to present a new methodology to model a generic low-level flight close to terrain, which guarantees terrain collision avoidance. Benefiting the advantages of high-speed computer technology, this method uses satellite elevation maps to generate so called 'Quad-tree forms'. The latter is then used to find the optimal trajectories for low-level flights. The novelty of this approach, entitled the 'cost map', lies in the integration of aircraft dynamics into the segmented map. This procedure results in some near-optimal trajectories with respect to aircraft dynamics that could easily be used for minimization of flight path together with pilot effort. Different... 

    Some sufficient conditions for the intersection with the vertical isocline in the Liénard plane

    , Article Applied Mathematics Letters ; Volume 19, Issue 5 , 2006 , Pages 491-497 ; 08939659 (ISSN) Aghajani, A ; Moradifam, A ; Sharif University of Technology
    2006
    Abstract
    In this work we study the problem of whether all trajectories of the system ẋ=y-F(x) and ẏ=-g(x) cross the vertical isocline, which is very important for the existence of periodic solutions and oscillation theory. Sufficient conditions are given for all trajectories to cross the vertical isocline. © 2005 Elsevier Ltd. All rights reserved  

    On the dynamics of gravity-induced wave function reduction

    , Article International Journal of Modern Physics A ; Volume 36, Issue 26 , 2021 ; 0217751X (ISSN) Rahmani, F ; Golshani, M ; Sharif University of Technology
    World Scientific  2021
    Abstract
    In this study, we use the concept of Bohmian trajectories to present a dynamical and deterministic interpretation for the gravity-induced wave function reduction. We shall classify all possible regimes for the motion of a particle, based on the behavior of trajectories in the ensemble and under the influence of quantum and gravitational forces. In the usual approaches all the information is obtained from the wave function evolution. But, on the basis of Bohm's deterministic quantum theory, we can investigate the motion of the particle during the reduction processes. This leads to analytical and numerical results for the reduction time and equation of motion of the particle. In this regard, a... 

    A new application of multi-criteria decision making in identifying critical dust sources and comparing three common receptor-based models

    , Article Science of the Total Environment ; Volume 808 , 2022 ; 00489697 (ISSN) Hosseini Dehshiri, S. S ; Firoozabadi, B ; Afshin, H ; Sharif University of Technology
    Elsevier B.V  2022
    Abstract
    Dust storms are a common phenomenon in arid and semi-arid regions in West Asia, which has led to high levels of PM10 in local and remote area. The Yazd city in Iran with a high PM10 level located downstream of dust sources in the Middle East and Central Asia. In this study, based on meteorological and PM10 monitoring data, backward trajectory modeling of air parcels related to dust events at Yazd station was performed using the HYSPLIT model in 2012–2019. The trajectory cluster analysis was used to identify the main dust transport pathways and wind systems. Three methods of Cross-referencing Backward Trajectory (CBT), Potential Source Contribution Function (PSCF) and Concentration Weighted... 

    A neuro-optimal approach for thrust-insensitive trajectory planning

    , Article Aircraft Engineering and Aerospace Technology ; Volume 81, Issue 3 , 2009 , Pages 212-220 ; 00022667 (ISSN) Pourtakdoust, S. H ; Pazooki, F ; Noushabadi, F ; Sharif University of Technology
    2009
    Abstract
    Purpose - The purpose of this paper is to devise a new approach to synthesize closed-loop feedback guidance law for online thrust- insensitive optimal trajectory generation utilizing neural networks. Design/methodology/approach - The proposed methodology utilizes an open- loop variational formulation that initially determines optimal launch/ ascent trajectories for various scenarios of known uncertainties in the thrust profile of typical solid propellant engines. These open-loop optimized trajectories will then provide the knowledge base needed for the subsequent training of a neural network. The trained network could eventually produce thrust-insensitive closed-loop optimal guidance laws... 

    Optimal Trajectory Planning for Aircraft Microgravity Atmospheric Maneuver

    , M.Sc. Thesis Sharif University of Technology Saki, Reza (Author) ; Pourtakdoust, Hossein (Supervisor)
    Abstract
    The purpose of the current study is to design an optimal trajectory and control for an aircraft to perform a microgravity maneuver automatically. This subject is by itself an important research topic that has not yet been attempted via optimal control formulation and modelling. Space stations are commonly utilized to conduct long-term microgravity research. Unfortunately utility of space stations to perform space based microgravity experiments is expensive and inaccessible for many researchers and scientific institutions. However, since many experiments requiring microgravity conditions can be performed in short time intervals, there is a possibility to meet their demand via optimal... 

    Control of a Quadcopter for Rapid Descent

    , Ph.D. Dissertation Sharif University of Technology Talaeizadeh, Amin (Author) ; Alasty, Aria (Supervisor) ; Nejat Pishkenari, Hossein (Supervisor)
    Abstract
    It is well-known that helicopters descending fast may enter a region in the velocity space called Vortex Ring State where the blade’s lift differs significantly from regular regions and includes high amplitude fluctuations. These fluctuations may lead to instability and therefore, this region is avoided, typically by increasing the horizontal speed. However, this region is not fully identified for multirotors, which their blades are rigid in contrary of helicopter’s blades which have two degrees of freedom. This project researches this phenomenon in the context of small-scale quadcopters. The region corresponding to the VRS is identified by combining first-principles modeling and wind-tunnel... 

    Multi-objective optimization in graceful performance degradation and its application in spacecraft attitude fault-tolerant control

    , Article Aerospace Science and Technology ; Volume 69 , 2017 , Pages 465-473 ; 12709638 (ISSN) Moradi, R ; Alikhani, A ; Fathi Jegarkandib, M. F ; Sharif University of Technology
    Abstract
    Reducing the burden of the remaining actuators through decreasing the performance gracefully is an important field in active fault tolerant control. According to the literature, two important points have been identified in the works considering graceful performance degradation: 1) using single-objective optimization, 2) assuming an engineering insight into the performance of the faulty system. This paper has two contributions: First, it is shown that in some cases, single-objective optimization may not be able to provide a satisfactory solution for the problem. Second, a new systematic and general method is proposed to remove the need for the engineering insight. The proposed method is based... 

    Nonlinear optimal control of planar musculoskeletal arm model with minimum muscles stress criterion

    , Article Journal of Computational and Nonlinear Dynamics ; Volume 12, Issue 1 , 2017 ; 15551415 (ISSN) Sharifi, M ; Salarieh, H ; Behzadipour, S ; Sharif University of Technology
    American Society of Mechanical Engineers (ASME)  2017
    Abstract
    In this paper, the optimal performance of a planar humanlike musculoskeletal arm is investigated during reaching movements employing an optimal control policy. The initial and final states (position and velocity) are the only known data of the response trajectory. Two biomechanical objective functions are taken into account to be minimized as the central nervous system (CNS) strategy: (1) a quadratic function of muscle stresses (or forces), (2) total time of movement plus a quadratic function of muscle stresses. A two-degress of freedom (DOF) nonlinear musculoskeletal arm model (for planar movements) with six muscle actuators and four state variables is used in order to evaluate the proposed... 

    Dynamic modelling and control of a sphere-based micro robot with adjustable arm

    , Article MARSS 2018 - International Conference on Manipulation, Automation and Robotics at Small Scales, 4 July 2018 through 8 July 2018 ; 2018 ; 9781538648414 (ISBN) Esfandbod, A ; Nejat Pishkenari, H ; Meghdari, A ; Sharif University of Technology
    Abstract
    In this article, we propose a three-dimensional model of a low-Reynolds-number swimmer that consists of three small spheres connected to a larger sphere via three perpendicular adjustable rods which enable the micro robot to swim along arbitrary trajectories. Then we focus on dynamic modelling of the swimmer and propose a control method to control the position of the micro swimmer in a low Reynolds number flow. The control aim intended in this article is that the middle sphere to follow a desired trajectory and respective simulation results from control indicates successful accomplishment in application. © 2018 IEEE  

    A disambiguation technique for passive localization using trajectory analysis

    , Article IEEE Transactions on Aerospace and Electronic Systems ; 2018 ; 00189251 (ISSN) Samizadeh Nikoo, M ; Behnia, F ; Sharif University of Technology
    Abstract
    In some well-known passive localization methods, when the number of equations equals the number of unknown object coordinates, there arise finite number of possible solutions. A localization disambiguation technique is required to identify the correct solution in these cases. As an example, the exact solution of time-difference-of-arrival (TDOA) based equations for four receiver sites, leads to a couple of solutions with only one of them being the true target position. This ambiguity, conventionally is resolved by using angle-of-arrival (AOA) measurements or using an additional receiver site which increase the cost and complexity of the system. In this paper a localization disambiguation... 

    The control of electron quantum trajectories on the high-order harmonic generation of CO and N2 molecules in the presence of a low frequency field

    , Article Journal of Chemical Physics ; Volume 148, Issue 14 , 2018 ; 00219606 (ISSN) Koushki, A. M ; Sadighi Bonabi, R ; Mohsen Nia, M ; Irani, E ; Sharif University of Technology
    American Institute of Physics Inc  2018
    Abstract
    In the present work, an efficient method is theoretically investigated for extending high-order harmonics and ultrashort attosecond pulse generation in N2 and CO molecules by using the time-dependent density functional theory approach. Our results show that by utilizing chirped laser field in the presence of a low frequency field, not only is the harmonic cutoff extended remarkably but also the single short quantum trajectory is selected to contribute to the harmonic spectra. When a low frequency field is added to the two-color chirped laser field, the long quantum trajectories are suppressed and only the short quantum trajectories contribute to the higher harmonic emission mechanism. As a... 

    A guidance algorithm for launch to equatorial orbit

    , Article Aircraft Engineering and Aerospace Technology ; Volume 81, Issue 2 , 2009 , Pages 137-148 ; 00022667 (ISSN) Marrdonny, M ; Mobed, M ; Sharif University of Technology
    2009
    Abstract
    Purpose - The purpose of this paper is to propose a new guidance algorithm for launching a satellite using an expendable rocket from an equatorial site to an equatorial low-Earth orbit. Design/methodology/approach - Guidance during endoatmospheric portion is based on a nominal trajectory computed prior to take-off. A set of updating computations begins anew at the time instant tg of transition from endoatmosphere to exoatmosphere. The updating computations determine a guidance trajectory and an associated control law for the remainder of path by taking into account the rocket state at time tg. Thus, the overall guidance involves both initial and midcourse operations, and it has both open-... 

    Particle trajectory study in submerged flows with baffles using v 2̄ - f and k -ε turbulence models

    , Article 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 7 January 2008 through 10 January 2008 ; 2008 ; 9781563479373 (ISBN) Mehdizadeh Momen, A ; Sherif, A ; Firoozabadi, B ; Sharif University of Technology
    2008
    Abstract
    In this paper, the structure of a wall jet deflected by a baffle along with the trajectory of particles has been studied. This baffle is used to produce a stable deflected surface jet, thereby deflecting the high-velocity supercritical stream away from the bed to the surface. An elliptic relaxation turbulence model (v2̄ - f model) has been used to simulate this submerged flow. During the last few years, the v2̄ - f turbulence model has become increasingly popular due to its ability to account for near-wall damping without use of damping functions. In addition, it has been proven that the v2̄ - f model is superior to other RANS methods in many fluid flows where complex flow features are... 

    Combinational hough transform for surveillance radar target detection in a 3-D data map

    , Article 2008 IEEE Radar Conference, RADAR 2008, Rome, 26 May 2008 through 30 May 2008 ; 2008 ; 9781424415397 (ISBN) Moqiseh, A ; Nayebi, M. M ; Sharif University of Technology
    2008
    Abstract
    A new method based on Hough transform is introduced for detection of linear trajectories in a 3-D data space. Data space is constructed from returned radar data using range, bearing, and time information. This information is then mapped into a 3-D Cartesian data space. The near constant velocity target trajectories appear as straight lines in this space, and are detected by the usage of the new method which is based on two 2-D Hough transforms in the bearing-time and range-time data spaces. The efficacy of this Combinational Hough transform method is verified by simulation and shown that it has a better performance, as compared with one 2-D data map case, where only uses the range-time... 

    3-D hough transform for surveillance radar target detection

    , Article 2008 IEEE Radar Conference, RADAR 2008, Rome, 26 May 2008 through 30 May 2008 ; 2008 ; 9781424415397 (ISBN) Moqiseh, A ; Nayebi, M. M ; Sharif University of Technology
    2008
    Abstract
    A 3-D Hough transform is introduced for detection of linear trajectories in a 3-D data space. Data space is constructed from returned radar data using range, bearing, and time information. This information is then mapped into a 3-D Cartesian data space. The constant velocity target trajectories appear as straight lines in this space, and are detected by the usage of 3-D Hough transform. The efficacy of the 3-D Hough transform is verified by simulation. In comparison with the 2-D case, when only the range-time information is used, the 3-D Hough transform has a better performance. © 2008 IEEE  

    Trajectory following of a micro motion stage based on closedloop fem simulation

    , Article ASME 2007 International Mechanical Engineering Congress and Exposition, IMECE 2007, 11 November 2007 through 15 November 2007 ; Volume 11 , 2007 , Pages 155-158 ; 079184305X (ISBN) Shahidi, A ; Mahboobi, S. H ; Pirouzpanah, S ; Esteki, H ; Sarkar, S ; ASME ; Sharif University of Technology
    American Society of Mechanical Engineers (ASME)  2007
    Abstract
    Micro motion stages are one of the essential components in field of micro robotics and ultra fine positioning systems. This research presents the optimum design of a 3-DOF micro motion stage and its position control using FEM simulation. This stage to be studied uses a 3 RRR flexure hinge base compliant mechanism driven by three piezoelectric stack actuators to provide micro scale planar motion. First of all parametric modeling of the stage will be fulfilled in ANSYS environment utilizing a commercial piezostack and different types of flexure hinges. Hence the Jacobian matrix will be achieved for each case. The optimum selection of the hinge form will be achieved upon results of the previous... 

    Minimum-Distance Collision-Free Trajectory Generation for Formation Flying Satellites Using a Hybrid Path-Planning Algorithm

    , M.Sc. Thesis Sharif University of Technology Behzadpour, Saniya (Author) ; Banazadeh, Afshin (Supervisor)
    Abstract
    The formation flight of satellites corresponds to a group of small satellites, performing the mission of a presumed larger and more expensive satellite. Usually mission designers tend to put these satellites in such orbital configurations that their trajectories do not intersect. Although a stable configuration in a certain collision-free orbit is desirable for long term purposes, most of the missions including maneuvers like forming or changing a configuration and inserting new satellites need to be planned using a proper path planning algorithm. In this thesis, a path planning algorithm is suggested that acquires the optimal and impact-free trajectories for a group of satellites for... 

    Optimal Sensors Placement for Passive Source Localization Considering NLOS Conditions

    , M.Sc. Thesis Sharif University of Technology Solhi Jouybari, Mohammad (Author) ; Behnia, Fereidoon (Supervisor)
    Abstract
    Passive Location is to obtain the location and velocity of a radio source using a source-generated signal in the environment and extract its parameters, which today have many applications in controlling security activities, tracking people and vehicles, emergency services, radar, Sonar, electronic warfare, and etc. . The location of a source is obtained by using a variety of methods such as received signal strength (RSS), signal angle of arrival (AOA), signal time of arrival (TOA), time difference of arrival (TDOA), and frequency difference of arrival (FDOA) of received signals. Many studies have been done in measuring and extracting data and solving the equations. However, little research... 

    Optimal Satellite Aided Capture of Spacecraft Around Jupiter

    , M.Sc. Thesis Sharif University of Technology Rasoulzadeh Darabad, Ali (Author) ; Asadian, Nima (Supervisor)
    Abstract
    In this thesis, satellite aided capture of spacecraft around Jupiter is optimized with the final goal of capture into a circular orbit around Europa. The cost functions of the multi-objective optimization process that should be minimized are: 1) summation of the propulsive ΔVs, 2) the total duration of the capture scenario, and 3) the integral flux of the energetic electrons and protons during the maneuvers. In this study, the spacecraft trajectory is modeled by patched conics method and is optimized by metaheuristic methods of genetic algorithm and simulated annealing. In some cases, interior point method is used for improving the final converged solution. Due to the limitations of...