| Attitude control of an underactuated spacecraft using tube-based MPC approach M Mirshams, M Khosrojerdi Aerospace Science and Technology 48, 140-145, 2016 | 50 | 2016 |
| Design and manufacturing of a research magnetic torquer rod MF Mehrjardi, M Mirshams Fourth International Conference on Experimental Mechanics 7522, 543-549, 2010 | 47 | 2010 |
| Collaborative optimization of remote sensing small satellite mission using genetic algorithms A Jafarsalehi, PM Zadeh, M Mirshams Iranian Journal of Science and Technology. Transactions of Mechanical …, 2012 | 31 | 2012 |
| Numerical and experimental investigation of vortex breaker effectiveness on the improvement in launch vehicle ballistic parameters MN Mahyari, H Karimi, H Naseh, M Mirshams Journal of Mechanical Science and Technology 24, 1997-2006, 2010 | 30 | 2010 |
| 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 |
| Passive fault-tolerant sliding mode attitude control for flexible spacecraft with faulty thrusters M Mirshams, M Khosrojerdi, M Hasani Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2014 | 26 | 2014 |
| Minimum-time optimal control of flexible spacecraft for rotational maneuvering A Ebrahimi, SAA Moosavian, M Mirshams Proceedings of the 2004 IEEE International Conference on Control …, 2004 | 24 | 2004 |
| Multi-objective multidisciplinary design of space launch system using holistic concurrent design M Mirshams, H Naseh, HR Fazeley Aerospace Science and Technology 33 (1), 40-54, 2014 | 23 | 2014 |
| Pyramidal reaction wheel arrangement optimization of satellite attitude control subsystem for minimizing power consumption A Shirazi, M Mirshams International Journal of Aeronautical and Space Sciences 15 (2), 190-198, 2014 | 23 | 2014 |
| Conceptual remote sensing satellite design optimization under uncertainty A Jafarsalehi, HR Fazeley, M Mirshams Aerospace Science and Technology 55, 377-391, 2016 | 22 | 2016 |
| Attitude control of an underactuated spacecraft using quaternion feedback regulator and tube-based MPC M Mirshams, M Khosrojerdi Acta Astronautica 132, 143-149, 2017 | 20 | 2017 |
| 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 |
| Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea M Mirshams, H Karimi, H Naseh Journal of Space Science and Technology 1 (2), 2008 | 17 | 2008 |
| Dynamics of space free-flying robots with flexible appendages A Ebrahimi, SAA MOUSAVIAN JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST) 4 (4), 29-36, 2007 | 17* | 2007 |
| Mass properties identification and automatic mass balancing system for satellite attitude dynamics simulator G Sharifi, M Mirshams, H Shahmohamadi Ousaloo Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2019 | 15 | 2019 |
| Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters M Mirshams, H Karimi, H Naseh Space Science and Technology 1 (1), 21-36, 2008 | 15 | 2008 |
| 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 |
| Statistical model of power supply subsystem Satellite M Mirshams, E Zabihian, AR Zabihian 2013 6th international conference on recent advances in space technologies …, 2013 | 12 | 2013 |
| 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 |
| LAUNCH VEHICLE COLLABORATIVE ROBUST OPTIMAL DESIGN WITH MULTI OBJECTIVE ASPECT AND UNCERTAINTIES M Mirshams, J Roshanian, DS YADEGARI, AA Bataleblu Modares Mechanical Engineering 15 (11), 339-350, 2016 | 10 | 2016 |
Hassan NasehAerospace Research Institute (ARI), Ministry of Science, Research and Technology (MSRT)在 ari.ac.ir 的电子邮件经过验证
