| 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 | 21 | 2018 |
| 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 | 7 | 2017 |
| 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 | 7 | 2014 |
| Multi-objective optimization of orbit transfer trajectory using imperialist competitive algorithm A Shirazi 2017 IEEE Aerospace Conference, 1-14, 2017 | 6 | 2017 |
| 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 | 5 | 2015 |
| Trajectory optimization of spacecraft high-thrust orbit transfer using a modified evolutionary algorithm A Shirazi Engineering Optimization 48 (10), 1639-1657, 2016 | 4 | 2016 |
| 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 | 4 | 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 | 3 | 2016 |
| Software Development for Satellite Thermal Design A Shirazi, M Mirshams Applied Mechanics and Materials 390, 703-707, 2013 | 3 | 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 | 1 | 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 | | 2019 |
| Optimal multi-impulse space rendezvous considering limited impulse using a discretized Lambert problem combined with evolutionary algorithms A Shirazi, J Ceberio, JA Lozano | | 2019 |
Jose A. LozanoU. of the Basque Country, Basque Center for Applied Mathematics, Research Associate at Sherpa.aiVerified email at ehu.es
