| A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system HR Fazeley, H Taei, H Naseh, M Mirshams Structural and Multidisciplinary Optimization 53, 145-160, 2016 | 26 | 2016 |
| Spacecraft attitude dynamics simulator actuated by cold gas propulsion system M Mirshams, H Taei, M Ghobadi, H Haghi Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2015 | 18 | 2015 |
| Liquid propellant engine conceptual design by using a fuzzy-multi-objective genetic algorithm (MOGA) optimization method M Mirshams, H Naseh, H Taei, HR Fazeley Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2014 | 12 | 2014 |
| Using air-bearing based platform and cold gas thruster actuator for satellite attitude dynamics simulation. M Mirshams, M Ghobadi, H Haghi, G Sharifi Modares Mechanical Engineering 14 (12), 2015 | 11 | 2015 |
| Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels حجت طائی, حجت, میرشمس, مهران, قبادی, وحید دستگردی, محمد امین, حقی, حسن علوم و فناوری فضایی 8 (4), 35-44, 2016 | 9 | 2016 |
| A systems engineering tool for satellite simulator design M Mirshams, MA Vahid D, H Taei Engineering Systems Design and Analysis 49194, 475-483, 2010 | 7 | 2010 |
| A 3‐DOF SATELLITE SIMULATOR DESIGN AND DEVELOPMENT M Mirshams, H Taei, A Novin-zadeh, F Ebadi International Aerospace Congress, 2009 | 6 | 2009 |
| A 6-DoF satellite virtual simulator design and development M Mirshams, A Nahvi, M Khosrojerdi, H Tae, A Vahid Applied Mechanics and Materials 186, 70-74, 2012 | 5 | 2012 |
| Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results H Taei, M Hozuri, A Adami Space Science and Technology 10 (2), 53-63, 2017 | 2 | 2017 |
| Optimal Design Layout for a Tri-axial Satellite Attitude Dynamics Simulator with Combinatorial Actuators H Taei K. N. Toosi University of Technology, 2015 | 2* | 2015 |
| Design and Manufacturing of a Tri-axial Spacecraft Attitude Motion Simulator M Mirshams, H Taei, H Haghi, V Rezvani Flight Simulation (FSIM) Conference, 2009 | 2 | 2009 |
| Applying multi-objective optimization approaches to design an optimal controller for orbital docking by consideration of actuators dynamics and comparing results H Taei, P Shokrolahi Space Science and Technology 13 (2), 87-96, 2020 | 1 | 2020 |
| Survey of hardware-based satellite attitude dynamics simulators H Taei Aerospace Knowledge and Technology Journal 6 (2), 87-101, 2017 | 1 | 2017 |
| به‌کارگیری رویکردهای محاسبات نرم برای توسعه یک رهیافت مهندسی همزمان در طراحی پیکره‌بندی یک پهپاد طائی, حجت, عزیزی, مهرانعلی, حقیقت اصفهانی, محمود, ستاینده دانش و فناوری هوافضا 12 (1), 43-62, 2023 | | 2023 |
| Application of soft computing methodologies for development of a concurrent engineering approach in design of UAV configuration H Taei, MA Azizi, M Haghighat E, SMR Setayandeh Aerospace Knowledge and Technology Journal 12 (1), 43-62, 2023 | | 2023 |
| Control Allocation Based on Fuzzy Approach for Landing Phase of Specific Aircraft H TAEI, S Nikseresht, A Babaee AEROSPACE MECHANICS JOURNAL, 2023 | | 2023 |
| Robust PID Control for Flexible Satellite Considering Dynamics of Thruster Actuator H Taei, S Ayati, SF Mousavi Iranian Journal of Mechanical Engineering Transactions of ISME 24 (3), 94-119, 2022 | | 2022 |
| Robust H∞ Control Design for Thrust Vectoring System of a UAV H Taei, A Aboutalebiyan Technology in Aerospace Engineering 6 (1), 17-28, 2022 | | 2022 |
| طراحی چندموضوعی سامانه پیشرانش دومولفه‌ای به سه روش بهینه، مبتنی بر قابلیت اطمینان و بهینه مبتنی بر قابلیت اطمینان طائی, حجت, آدمی, حضوری, منصور علوم و فناوری فضایی 14 (4), 85-98, 2021 | | 2021 |
| Multidisciplinary Design of Bipropellant Propulsion System in Three Methods, Optimal Design, Reliability Based Design and Optimal Reliability Based Design H Taei, A Adami, M Hozuri Space Science and Technology 14 (4), 85-98, 2021 | | 2021 |
