Spacecraft reentry trajectory optimization by heuristic optimization methods and optimal control theory von Ekrami Kivaj, Alireza, Basohbat Novinzadeh, Alireza, Pazooki, Farshad

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On the Performance of the Model-Free Adaptive Control For A Novel Moving-Mass Controlled Flying Robot von Heydari, Mohsen, Darvishpoor, Shahin, Novinzadeh, Alireza Basohbat, Roshanian, Jafar

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Designing a closed-loop guidance system to increase the accuracy of satellite-carrier boosters' landing point von Tavakoli, Farhad, Novinzadeh, Alireza Basohbat

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An analytical guidance law of planetary landing mission by minimizing the control effort expenditure von Afshari, Hamed Hossein, Novinzadeh, Alireza Basohbat, Roshanian, Jafar

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Satellite constellation build-up via three-body dynamics von Nadoushan, Mahdi Jafari, Novinzadeh, Alireza Basohbat

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Solid upper stage design process using finite burn maneuvers for low Earth orbit–geosynchronous Earth orbit transfer phase von Motlagh, Javad Amiri, Novinzadeh, Alireza Basohbat

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Dynamic analysis of a nonlinear pressure regulator using bondgraph simulation technique von Afshari, Hamed Hossein, Zanj, Amir, Novinzadeh, Alireza Basohbat

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Determination of Nonlinear Optimal Feedback Law for Satellite Injection Problem Using Neighboring Optimal Control von Afshari, Hamed Hossein, Novinzadeh, Alireza Basohbat, Roshanian, Jafar

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New approach in designing solid upper stage for interplanetary missions using finite burn assumption von Motlagh, Javad Amiri, Novinzadeh, Alireza Basohbat, Zakeri, Mostafa

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