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Mehran Mirshams
Mehran Mirshams
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Titel
Zitiert von
Zitiert von
Jahr
Attitude control of an underactuated spacecraft using tube-based MPC approach
M Mirshams, M Khosrojerdi
Aerospace Science and Technology 48, 140-145, 2016
482016
Design and manufacturing of a research magnetic torquer rod
MF Mehrjardi, M Mirshams
Fourth International Conference on Experimental Mechanics 7522, 543-549, 2010
442010
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
312012
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
302010
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
252016
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
252014
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
242004
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
232014
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
232014
Conceptual remote sensing satellite design optimization under uncertainty
A Jafarsalehi, HR Fazeley, M Mirshams
Aerospace Science and Technology 55, 377-391, 2016
222016
Attitude control of an underactuated spacecraft using quaternion feedback regulator and tube-based MPC
M Mirshams, M Khosrojerdi
Acta Astronautica 132, 143-149, 2017
192017
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
182015
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
172008
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
142019
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
142008
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
122014
Statistical model of power supply subsystem Satellite
M Mirshams, E Zabihian, AR Zabihian
2013 6th international conference on recent advances in space technologies …, 2013
122013
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
112015
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
102016
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