Segui
Mehran Mirshams
Titolo
Citata da
Citata da
Anno
Attitude control of an underactuated spacecraft using tube-based MPC approach
M Mirshams, M Khosrojerdi
Aerospace Science and Technology 48, 140-145, 2016
542016
Design and manufacturing of a research magnetic torquer rod
MF Mehrjardi, M Mirshams
Fourth International Conference on Experimental Mechanics 7522, 543-549, 2010
472010
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
332010
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
Conceptual remote sensing satellite design optimization under uncertainty
A Jafarsalehi, HR Fazeley, M Mirshams
Aerospace Science and Technology 55, 377-391, 2016
272016
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
272014
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
262016
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
262014
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
262014
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
Attitude control of an underactuated spacecraft using quaternion feedback regulator and tube-based MPC
M Mirshams, M Khosrojerdi
Acta Astronautica 132, 143-149, 2017
212017
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
182019
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), 17-25, 2008
182008
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
162008
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
16*2007
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
132014
Design and performance simulation of a satellite momentum exchange actuator
A Shirazi, M Mirshams
Australian Journal of Mechanical Engineering 14 (1), 1-9, 2016
122016
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
Launch vehicle collaborative robust optimal design with multiobjective aspect and uncertainties
M Mirshams, J Roshanian, S Yadegari Dehkordi, AA Bataleblu
Modares Mechanical Engineering 15 (11), 339-350, 2016
112016
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
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