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s m esmaeilzadeh
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Attitude control of a quadrotor with optimized PID controller
H Bolandi, M Rezaei, R Mohsenipour, H Nemati, SM Smailzadeh
Intelligent Control and Automation 2013, 2013
2912013
Chattering-free fault-tolerant attitude control with fast fixed-time convergence for flexible spacecraft
SM Esmaeilzadeh, M Golestani, S Mobayen
International Journal of Control, Automation and Systems 19, 767-776, 2021
542021
Fixed-time control for high-precision attitude stabilization of flexible spacecraft
M Golestani, SM Esmaeilzadeh, S Mobayen
European Journal of Control 57, 222-231, 2021
472021
Finite‐time fault‐tolerant adaptive robust control for a class of uncertain non‐linear systems with saturation constraints using integral backstepping approach
SM Smaeilzadeh, M Golestani
IET Control Theory & Applications 12 (15), 2109-2117, 2018
412018
Model predictive control of attitude maneuver of a geostationary flexible satellite based on genetic algorithm
M TayyebTaher, SM Esmaeilzadeh
Advances in Space research 60 (1), 57-64, 2017
362017
A finite-time adaptive robust control for a spacecraft attitude control considering actuator fault and saturation with reduced steady-state error
SM Smaeilzadeh, M Golestani
Transactions of the Institute of Measurement and Control 41 (4), 1002-1009, 2019
302019
Constrained attitude control for flexible spacecraft: Attitude pointing accuracy and pointing stability improvement
M Golestani, M Esmaeilzadeh, S Mobayen
IEEE Transactions on Systems, Man, and Cybernetics: Systems 53 (3), 1566-1572, 2022
162022
Modeling and co-simulating of a large flexible satellites with three reaction wheels in ADAMS and MATLAB
M Tahmasebi, SM Esmailzadeh
International Journal of Dynamics and Control 6, 79-88, 2018
162018
Fault-tolerant attitude control for flexible spacecraft subject to input and state constraint
M Golestani, SM Esmaeilzadeh, B Xiao
Transactions of the Institute of Measurement and Control 42 (14), 2660-2674, 2020
132020
Estimation of Simplified General Perturbations model 4 orbital elements from global positioning system data by invasive weed optimization algorithm
ME H Bolandi, MH Ashtari Larki, SH Sedighy, MS Zeighami
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2015
132015
Comment on “fixed-time attitude control for rigid spacecraft with actuator saturation and faults”
SM Esmailzadeh, M Golestani
IEEE Transactions on Control Systems Technology 27 (4), 1846-1846, 2018
122018
Analytical modelling and nonlinear strain feedback control of a flexible robot ARM
H Bolandi, SM Esmaeilzadeh
Automatic Control and Computer Sciences 42, 236-248, 2008
92008
Adaptive attitude stabilization of flexible spacecraft with fast fixed-time convergence
SM Esmaeilzadeh, M Golestani, A Fekih
Iranian Journal of Science and Technology, Transactions of Mechanical …, 2022
72022
GPS based onboard orbit determination system providing fault management features for a LEO satellite
H Bolandi, MHA Larki, M Abedi, M Esmailzade
The Journal of Navigation 66 (4), 539-559, 2013
72013
Exact tip trajectory tracking control of a flexible robot arm
H Bolandi, SM Esmaeilzadeh
International Journal of Robotics and Automation 26 (1), 100, 2011
42011
A new obstacle avoidance algorithm for quad rotors group in the presence of dynamic and static obstacles
M Rezaei, H Bolandi, F Jamaldoost, SM Smailzadeh
Cumhuriyet Üniversitesi Fen Edebiyat Fakültesi Fen Bilimleri Dergisi 36 (3 …, 2015
32015
Implementation of an AMR magnetic sensor by means of a microcontroller to achieve more accurate response
H Bolandi, N Riahi, M Esmaeilzadeh, M Abedi, B Ghorbani
2013 21st Iranian Conference on Electrical Engineering (ICEE), 1-5, 2013
32013
Adaptive Nonlinear Sensor Output Feedback Control of a Flexible Robot Arm
H Bolandi, SM Esmaeilzadeh
2008 International Conference on Computer and Electrical Engineering, 639-647, 2008
32008
Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm
M Hashemi, SK Mosavi Mashhadi, SM Smaeilzadeh, M Fiuzy
Journal of Space Science and Technology (JSST) 9 (2), 85-90, 2016
22016
Analysis of Navi satellite TLEs and its effect of tracking by ground station
H Bolandi, MH Ashtrai, M Nadi, SM Esmaeilzadeh
JSST 6 (2), 2013
22013
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