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Alireza Toloei

Associate Professor

Update: 2024-05-16

Alireza Toloei

New technologies and aerospace engineering /

M.Sc. Theses

  1. Design and Implementation of Automatic Charger and Flying Robot Auto Pilot
    Amir Kian 2021
  2. predictive controller design for manpad missile with proportional ofnavigation
    Mohammadamin Malekian 2020
  3. Catalog’s search methods in stellar navigation.
    Asieh Salehi 2020
  4. Control of Atmospheric Reentry Vehicle with Moving Mass Actuator
    Mohammad Ali Ansari Jafari 2019
  5. Numerical flow simulation on jet vanes in order to transfer pitch program differeniated pattern based on 3 degrees of freedom simulation in space launch vehicle
    Khashayar Jamal ashtiani 2019
  6. Formation control of multiple quadrotor using leader-follower approach
    Marzieh Habibi totekani 2019
  7. Orbital Transfer Simulation of Low-Thrust Spacecraft with Electric Propulsion
    Alidad Ghasser 2019

  8. Asef Raoufi 2019
  9. Simulation and Analysis of Proportional Navigation , Pursuit and Differential Geometry in Missile Equipped with Two-Gimbaled Seeker
    Mahdi Torabi 2019

  10. Reza Saghandian Tousi 2018

  11. Hooman Asgari 2018

  12. MOHAMMADREZA KHAJEHSARVI 2018

  13. Atefeh Azadeh 2018

  14. Jalaledin Sajjadi 2017

  15. Reihaneh Sahebi Sharif Abadi 2016

  16. Abolfazl Rezaee Nezhad Eshkuri 2016

  17. Akram Bayat 2016

  18. Elaheh Aghamirbaha 2016

  19. SHIMA SHAHABODDIN 2016
  20. Transient Flow Simulation with Secondary Injection for Thrust Vector Control
    HAMID RAMEZI 2016
  21. Adaptive controller design during automatic landing phase of aircraft in the presence of external disturbances
    Mohammad Hadi Mollaei Renani 2016
  22. Autopilot Design for Unmanned Aerial Vehicles by sliding mode control
    MOHSEN HOSSEINZADEH DAVIL 2015
  23. Flow simulation for dual secondary injection in order to introduce two conveninent hole locations in thrust vector control
    Afshin Rohanirad 2015
  24. Designing optimal Trajectory of Surface to Air Missile Based on Simulation with Genetic optimization Algorithm
    Rasoul Hesami Rostami 2015
  25. Designing Optimal Trajectory in presence of Terrain and Threat for Unmanned Aerial Vehicles Using Evolutionary Algorithm
    Alireza Dayhim 2015

  26. Masoumeh Eslamdoust 2015
  27. Nonlinear Controller Design For Airplane Automatic Landing System Using ILS/GPS Navigation
    Seyedesoha Javanbakht 2015

  28. Reza Saboori 2015

  29. 2014

  30. 2014

  31. 2014

  32. 2014
  33. Nonlinear Controller Design for Aircraft Suspension System with Semi Active Control and Intelligent Optimization
    2014

  34. 2014

  35. 2014

  36. 2014

  37. 2014

  38. Morteza Shayanarani 2014

  39. Hamidreza Shahsavari 2013

  40. MOHSEN GILANIFAR 2013
  41. SATELLITE LIFETIME ANALYTICAL SEMIANALYTICAL NUMERICAL FOR LEO WITH PERTURBATION BY PROGRAM MATLAB
    Mohammadreza Sahebi 2012
  42. Effects Analysis of Frozen Orbits in Modeling of Relative Motion Dynamics between Two Spacecrafts
    Ahmad Soleymani 2012
  43. Performance Evaluation of theHigh Altitude Launch Techniques to Orbit Using Atmospheric Properties
    MOHAMMAD REZA TAHERI 2012
  44. 6DOF Dynamic Aerodynamic Coupled Simulation of a Launch Vehicle Parallel Boosters Separation
    2012

  45. 2011

  46. 2011
  47. Optimal Pitch Program Algorithm For Launch Vehicle
    Elyas Mohajeri 2010
  48. An Approximate Solution of Viscous Flow about Blunted Nosed Bodise and Aerodynamic Rate Calulation
    2010
  49. Inviscid solution around axisymmetric body in the hypersonic flow
    2010

  50. Seyedmohammadreza Mahmoodian 2010

  51. 2010
  52. Multidisciplinary design optimization of a solid propellant Launch Vehicle
    2010
  53. automatic star identification using traingle base
    2010
  54. Multidisciplinarv design optimization of launch vehicle
    2010
  55. Flow Simulation of Multiple Injection for Fluidic Thrust Vectoring
    2010
  56. Simulation of the Electrostatic and Magnetic Field on Produts of Combustion in Chemical Thrusters
    Mahmoud Dehghani 2010