| Simultaneous optimization of staging and trajectory of launch vehicles using two different approaches R Jamilnia, A Naghash Aerospace Science and Technology 23 (1), 85-92, 2012 | 38 | 2012 |
| A robust nonlinear control approach for tip position tracking of flexible spacecraft M Malekzadeh, A Naghash, HA Talebi IEEE Transactions on Aerospace and Electronic Systems 47 (4), 2423-2434, 2011 | 35 | 2011 |
| 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 | 34 | 2008 |
| Optimal guidance based on receding horizon control and online trajectory optimization R Jamilnia, A Naghash Journal of Aerospace Engineering 26 (4), 786-793, 2013 | 25 | 2013 |
| Robust attitude and vibration control of a nonlinear flexible spacecraft M Malekzadeh, A Naghash, HA Talebi Asian Journal of Control 14 (2), 553-563, 2012 | 21 | 2012 |
| Robust optimization of impulsive orbit transfers under actuation uncertainties MS Mohammadi, A Naghash Aerospace Science and Technology 85, 246-258, 2019 | 17 | 2019 |
| Control of flexible spacecraft using dynamic inversion and µ-synthesis M Malekzadeh, A Naghash, HA Talebi Journal of Vibration and Control 17 (13), 1938-1951, 2011 | 16 | 2011 |
| Cost evaluation of different snatch trajectories by using dynamic programming method SL Nejadian, M Rostami, A Naghash Procedia Engineering 2 (2), 2563-2567, 2010 | 16 | 2010 |
| Pitch and flight path controller design for F-16 aircraft using combination of LQR and EA techniques MR Mortazavi, A Naghash Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2018 | 11 | 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 control of non-linear flexible spacecraft M Malekzadeh, A Naghash, HA Talebi Scientia Iranica 17 (3), 2010 | 9 | 2010 |
| Precision approach with curved flight path and accurate time of arrival A Naghash, D Enns Guidance, Navigation, and Control Conference and Exhibit, 4207, 1998 | 9 | 1998 |
| Minimum time trajectory optimization for flying a quadrotor in an 8-shaped path A Naghash, M Naghshineh, A Honari International Micro Air Vehicle Conference, 17-20, 2013 | 7 | 2013 |
| Trajectory optimization of space manipulators with flexible links using a new approach M Bahrami, R Jamilnia, A Naghash INTERNATIONAL JOURNAL OF ROBOTICS 1 (1), 48-55, 2009 | 7 | 2009 |
| 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 |
| Comparison of back stepping optimized via PSO algorithm and LQR controllers for a quadrotor N Parhizkar, A Naghash Modares Mechanical Engineering 17 (7), 413-420, 2017 | 6 | 2017 |
| Flexible spacecraft control using robust feedback linearization M Malekzadeh, A Naghash, A Talebi AIAA Guidance, Navigation, and Control Conference, 8295, 2013 | 6 | 2013 |
| Incremental Predictive Command of Velocity to Be Gained Guidance Method NA GHAHRAMANI, A Naghash, F TOUHIDKHAH JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST) 5 (3), 99-105, 2008 | 6 | 2008 |
| Hybrid trajectory optimization using genetic algorithms R Esmaelzadeh, A Naghash, M Mortazavi Proceedings of the 1 st International Conference on Modeling, Simulation and …, 2005 | 6 | 2005 |
| Control and guidance of an autonomous quadrotor landing phase on a moving platform MA Isaac, A Naghash, S Mirtajedini Proceedings of the IMAV Annual Conference of Autonomous Vehicles, Madrid …, 2019 | 5 | 2019 |
