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Alireza Toloei

Associate Professor

Update: 2024-12-19

Alireza Toloei

New technologies and aerospace engineering /

P.H.D dissertations

  1. Generalized predictive formation control for heterogeneous multi-flying robots With obstacle avoidance: connectivity preservation approach
    Fatemeh Ghaderi 2024
  2. Laboratory simulation and implementation of the multi-field of view star sensor
    Mona Zahednamazi 2023
  3. Reliability-Based Robust Design Optimization Of Satellite Orbital Transfer System
    Mohammad Fatehi 2023

Master Theses

  1. design of air taxi aircraft with jet engine by evolutionary optimization method
    Hajar Shojaee mehr 2024
  2. The robust optimal design of a launch vehicle under uncertainty by Latin Hyper cube
    Mitra Ebrahimi 2023
  3. optimal design of robust remote sensing satellite by particle swarm method
    Fatemeh Ramezani 2023
  4. Optimal robust design of a cubic optical remote sensing satellite platform in Leo orbit.
    Saman Javadi kochaksaraii 2022
  5. Robust design for GEO telecommunication satellite
    Saeid Shafiei shahraki 2021
  6. Simulation and error analysis of the method for determining the attitude of the second-order optimal quaternion estimator in the star sensor
    Rashid Soltani 2021
  7. Simulation and implementation of the control system for an unmanned aircraft based on the flatness system technique
    Behnam Nakhodayegoli 2021
  8. H infinitive-based Leader-Follower Formation Control Design for Satellites Multi-Agent system
    Hadi Mostafaei 2021
  9. Design and Implementation of Automatic Charger and Flying Robot Auto Pilot
    Amir Kian 2021
  10. Catalog’s search methods in stellar navigation.
    Asieh Salehi 2020
  11. predictive controller design for manpad missile with proportional ofnavigation
    Mohammadamin Malekian 2020
  12. Control of Atmospheric Reentry Vehicle with Moving Mass Actuator
    Mohammad Ali Ansari Jafari 2019
  13. Formation control of multiple quadrotor using leader-follower approach
    Marzieh Habibi totekani 2019
  14. 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
  15. Orbital Transfer Simulation of Low-Thrust Spacecraft with Electric Propulsion
    Alidad Ghasser 2019
  16. Simulation and Analysis of Proportional Navigation , Pursuit and Differential Geometry in Missile Equipped with Two-Gimbaled Seeker
    Mahdi Torabi 2019

  17. Asef Raoufi 2019

  18. Reza Saghandian Tousi 2018

  19. Hooman Asgari 2018

  20. MOHAMMADREZA KHAJEHSARVI 2018

  21. Atefeh Azadeh 2018

  22. Jalaledin Sajjadi 2017

  23. Reihaneh Sahebi Sharif Abadi 2016

  24. Abolfazl Rezaee Nezhad Eshkuri 2016

  25. Akram Bayat 2016
  26. Transient Flow Simulation with Secondary Injection for Thrust Vector Control
    HAMID RAMEZI 2016

  27. SHIMA SHAHABODDIN 2016

  28. Elaheh Aghamirbaha 2016
  29. Adaptive controller design during automatic landing phase of aircraft in the presence of external disturbances
    Mohammad Hadi Mollaei Renani 2016
  30. Autopilot Design for Unmanned Aerial Vehicles by sliding mode control
    MOHSEN HOSSEINZADEH DAVIL 2015
  31. Flow simulation for dual secondary injection in order to introduce two conveninent hole locations in thrust vector control
    Afshin Rohanirad 2015
  32. Designing optimal Trajectory of Surface to Air Missile Based on Simulation with Genetic optimization Algorithm
    Rasoul Hesami Rostami 2015
  33. Designing Optimal Trajectory in presence of Terrain and Threat for Unmanned Aerial Vehicles Using Evolutionary Algorithm
    Alireza Dayhim 2015

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

  36. Reza Saboori 2015

  37. 2014

  38. 2014
  39. Nonlinear Controller Design for Aircraft Suspension System with Semi Active Control and Intelligent Optimization
    2014

  40. 2014

  41. 2014

  42. 2014

  43. 2014

  44. 2014

  45. Morteza Shayanarani 2014

  46. Hamidreza Shahsavari 2013

  47. MOHSEN GILANIFAR 2013
  48. SATELLITE LIFETIME ANALYTICAL SEMIANALYTICAL NUMERICAL FOR LEO WITH PERTURBATION BY PROGRAM MATLAB
    Mohammadreza Sahebi 2012
  49. Effects Analysis of Frozen Orbits in Modeling of Relative Motion Dynamics between Two Spacecrafts
    Ahmad Soleymani 2012
  50. Performance Evaluation of theHigh Altitude Launch Techniques to Orbit Using Atmospheric Properties
    MOHAMMAD REZA TAHERI 2012
  51. 6DOF Dynamic Aerodynamic Coupled Simulation of a Launch Vehicle Parallel Boosters Separation
    2012

  52. 2011

  53. 2011
  54. An Approximate Solution of Viscous Flow about Blunted Nosed Bodise and Aerodynamic Rate Calulation
    2010
  55. Optimal Pitch Program Algorithm For Launch Vehicle
    Elyas Mohajeri 2010
  56. Inviscid solution around axisymmetric body in the hypersonic flow
    2010

  57. Seyedmohammadreza Mahmoodian 2010

  58. 2010
  59. Multidisciplinary design optimization of a solid propellant Launch Vehicle
    2010
  60. automatic star identification using traingle base
    2010
  61. Multidisciplinarv design optimization of launch vehicle
    2010
  62. Flow Simulation of Multiple Injection for Fluidic Thrust Vectoring
    2010
  63. Simulation of the Electrostatic and Magnetic Field on Produts of Combustion in Chemical Thrusters
    Mahmoud Dehghani 2010