Abolfazl Shirazi
Abolfazl Shirazi
Ph.D Fellow, BCAM - Basque Center for Applied Mathematics
Verified email at bcamath.org - Homepage
Cited by
Cited by
Spacecraft trajectory optimization: A review of models, objectives, approaches and solutions
A Shirazi, J Ceberio, JA Lozano
Progress in Aerospace Sciences 102, 76-98, 2018
Attitude estimation and sensor identification utilizing nonlinear filters based on a low-cost MEMS magnetometer and sun sensor
MM Teshnizi, A Shirazi
IEEE Aerospace and Electronic Systems Magazine 30 (12), 20-33, 2015
Pyramidal reaction wheel arrangement optimization of satellite attitude control subsystem for minimizing power consumption
A Shirazi, M Mirshams
International Journal of Aeronautical and Space Sicences 15 (2), 190-198, 2014
Analysis of a hybrid genetic simulated annealing strategy applied in multi-objective optimization of orbital maneuvers
A Shirazi
IEEE Aerospace and Electronic Systems Magazine 32 (1), 6-22, 2017
Trajectory optimization of spacecraft high-thrust orbit transfer using a modified evolutionary algorithm
A Shirazi
Engineering Optimization 48 (10), 1639-1657, 2016
Multi-objective optimization of orbit transfer trajectory using imperialist competitive algorithm
A Shirazi
2017 IEEE Aerospace Conference, 1-14, 2017
Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission
A Shirazi, AH Mazinan
Computational and Applied Mathematics 35 (3), 865-879, 2016
Design and performance simulation of a satellite momentum exchange actuator
A Shirazi, M Mirshams
Australian Journal of Mechanical Engineering 14 (1), 1-9, 2016
Software Development for Satellite Thermal Design
A Shirazi, M Mirshams
Applied Mechanics and Materials 390, 703-707, 2013
Evolutionary algorithms to optimize low-thrust trajectory design in spacecraft orbital precession mission
A Shirazi, J Ceberio, JA Lozano
2017 IEEE Congress on Evolutionary Computation (CEC), 1779-1786, 2017
An evolutionary discretized Lambert approach for optimal long-range rendezvous considering impulse limit
A Shirazi, J Ceberio, JA Lozano
Aerospace Science and Technology 94, 105400, 2019
Optimal multi-impulse space rendezvous considering limited impulse using a discretized Lambert problem combined with evolutionary algorithms
A Shirazi, J Ceberio, JA Lozano
8th European Conference for Aeronautics and Space Sciences, 2019
The system can't perform the operation now. Try again later.
Articles 1–12