| Near optimal guidance law for descent to a point using inverse problem approach A Naghash, R Esmaelzadeh, M Mortazavi, R Jamilnia Aerospace Science and Technology 12 (3), 241-247, 2008 | 36 | 2008 |
| Control and synchronization chaotic satellite using active control SM Hamidzadeh, R Esmaelzadeh International journal of computer applications 94 (10), 2014 | 27 | 2014 |
| A new approach to trajectory optimization based on direct transcription and differential flatness MJ Poustini, R Esmaelzadeh, A Adami Acta Astronautica 107, 1-13, 2015 | 26 | 2015 |
| Appropriate starter for solving the Kepler’s equation R Esmaelzadeh, H Ghadiri International Journal of Computer Applications 975, 8887, 2014 | 17 | 2014 |
| Chaotic satellite synchronization using neural and nonlinear controllers SF Sarcheshmeh, R Esmaelzadeh, M Afshari Chaos, solitons & fractals 97, 19-27, 2017 | 16 | 2017 |
| Comparing fluid ring and CMG servomechanisms for active control of rigid satellites S Akbaritabar, R Esmaelzadeh, R Zardashti Aircraft Engineering and Aerospace Technology 90 (6), 896-905, 2018 | 13 | 2018 |
| An Explicit Reentry Guidance Law Using Bezier Curves R Esmaelzadeh, A Naghash, M Mortazavi Transactions of the Japan Society for Aeronautical and Space Sciences 50 …, 2008 | 10 | 2008 |
| Robust optimal attitude determination using interval analysis H Ghadiri, R Esmaelzadeh, R Zardashti Advances in Space Research 69 (6), 2611-2617, 2022 | 8 | 2022 |
| Low-thrust orbit transfer optimization using a combined method R Esmaelzadeh International Journal of Computer Applications 89 (4), 2014 | 8 | 2014 |
| Hybrid trajectory optimization using genetic algorithms R Esmaelzadeh, A Naghash, M Mortazavi Proceedings of the 1 st International Conference on Modeling, Simulation and …, 2005 | 8 | 2005 |
| Optimized fuzzy-quaternion attitude control of satellite in large maneuver H Ghadiri, M Sadeghi, A Abaspour, R Esmaelzadeh 14th International Conference on Space Operations, 2552, 2016 | 7 | 2016 |
| Near optimal re-entry guidance law using inverse problem approach R Esmaelzadeh, A Naghash, M Mortazavi Inverse Problems in Science and Engineering 16 (2), 187-198, 2008 | 7 | 2008 |
| Adjustable adaptive fuzzy attitude control using nonlinear SISO structure of satellite dynamics M Moradi, R Esmaelzadeh, A Ghasemi Transactions of the Japan Society for Aeronautical and Space Sciences 55 (5 …, 2012 | 4 | 2012 |
| Integrating second order sliding mode control and anomaly detection using auto-encoder for enhanced safety and reliability of quadrotor UAVs S Yazdannik, S Sanisales, M Tayefi, R Esmaelzadeh, M Khazaee International Journal of Reliability, Risk and Safety: Theory and …, 2022 | 3 | 2022 |
| Explicit Flatness-Based Guidance in Reentry Phase R Esmaelzadeh Space Science and Technology 6 (4), 29-36, 2014 | 2 | 2014 |
| On-board near optimal flight trajectory generation using deferential flatness R Esmaelzadeh International Journal of Computer Applications 89 (3), 2014 | 2 | 2014 |
| Artificial Intelligence Techniques for Spacecraft Health Monitoring System-A Survey S Sanisales, R Esmaelzadeh, M Khazaee The 21st International Conference of Iranian Aerospace Society. unknown, 2023 | 1 | 2023 |
| Review of Re-entry Guidance Methods Based on Trajectory Generation R Esmaelzadeh, FZ Rahmani Technology in Aerospace Engineering 5 (4), 61-72, 2022 | 1 | 2022 |
| Chaotic satellite synchronization using neural controllers S Farzami, R Esmaelzadeh, MR Taheri 2015 7th International Conference on Recent Advances in Space Technologies …, 2015 | 1 | 2015 |
| Atmospheric Re-Entry Control for Low Lift/Drag Vehicles A Ghasemi, MB Menhaj, R Esmaelzadeh, M Moradi | 1 | 2010 |
Abolghasem NaghashAssociate Professor在 aut.ac.ir 的电子邮件经过验证
