Follow
Ahmad Soleymani
Ahmad Soleymani
Researcher and PhD Candidate, Department of Aerospace Engineering, SBU and MUT
Verified email at mail.sbu.ac.ir
Title
Cited by
Cited by
Year
A comparative study of CMG and FMC actuators for nano satellite attitude control system-pyramidal configuration
J Tayebi, A Soleymani
2015 7th International Conference on Recent Advances in Space Technologies …, 2015
202015
Simulation of thermal distribution system of microsatellite equipped with FMC actuators
A Soleymani, M Nosratollahi
Aircraft Engineering and Aerospace Technology, 2020
92020
Modified L1 Adaptive Control Design for Satellite FMC Systems with Actuators Time Delay
M Nosratollahi, A Soleymani, SH Sadati
International Journal of Engineering 31 (11), 1982-1990, 2018
52018
Design of satellite's combined attitude and thermal control system equipped with FMC actuators
M Nosratolahi, A Soleymani, SH Sadati
Modares Mechanical Engineering 18 (1), 122-130, 2018
42018
Decision-Making System Design for Satellite Temperature Management in the Presence of Fluid Momentum Controller Actuators Fault
A Soleymani, M Nosratollahi, SH Sadati
Modares Mechanical Engineering 19 (4), 947-957, 2019
32019
Attitude Control System Design Based on Fluidic Momentum Controllers under Adaptive Sliding Mode
AH Taghavi, A Soleymani
Journal of Space Science and Technology (In Persian) 7 (2), 63-74, 2014
32014
Effect Analysis of Frozen Conditions for Spacecraft Relative Motion Dynamics
A Soleymani, AR Toloei
International Journal of Engineering-Transactions A: Basics 25 (4), 301, 2012
22012
High accuracy relative motion of spacecraft using linearized time-varying j2-perturbed terms
A Soleymani
International Journal of Engineering 26 (4), 323-332, 2013
12013
Performance Evaluation of the High-altitude Launch Technique to Orbit Using Atmospheric Properties
MR Taheri, A Soleymani, A Toloei, AR Vali
International Journal of Engineering-Transactions A: Basics 26 (4), 333, 2012
12012
Performance Analysis of FMC Actuators to Microsatellite Temperature Management Based on 3-Axis and Pyramidal Configuration
M NOSRATOLLAHI, A Soleimani
Journal of Space Science and Technology 13 (1), 49-60, 2020
2020
Spacecraft OMM reduction using stable frozen orbit conditions
A Soleymani, A Toloei
Aircraft Engineering and Aerospace Technology: An International Journal 87 …, 2015
2015
Structural Health Monitoring Based on Smart Fuzzy Network Using FEM Database
T Bahadorifard, A., Soleymani, A., Shojaee
The Proceedings of 14th Iranian Conferenceon Fuzzy Systems, 2014
2014
Inclusion Effects of J2-Perturbed Motion over Melton’s Problem
A Soleymani, A Toloei
Aircraft Engineering and Aerospace Technology 85 (3), 236-244, 2013
2013
Design of spacecraft attitude control algorithm for orbital maneuver phase based on maximum reliability
A Toloei, A Soleymani, MR Taheri
2013 6th International Conference on Recent Advances in Space Technologies …, 2013
2013
The system can't perform the operation now. Try again later.
Articles 1–14