| Repeat ground track orbit design with desired revisit time and optimal tilt MJ Nadoushan, N Assadian Aerospace Science and technology 40, 200-208, 2015 | 61 | 2015 |
| Investigation of thrust effect on the vibrational characteristics of flexible guided missiles SH Pourtakdoust, N Assadian Journal of sound and vibration 272 (1-2), 287-299, 2004 | 53 | 2004 |
| Multiobjective genetic optimization of Earth–Moon trajectories in the restricted four-body problem N Assadian, SH Pourtakdoust Advances in Space Research 45 (3), 398-409, 2010 | 49 | 2010 |
| Study of the triple-mass Tethered Satellite System under aerodynamic drag and J2 perturbations P Razzaghi, N Assadian Advances in Space Research 56 (10), 2141-2150, 2015 | 39 | 2015 |
| Robust distributed control of spacecraft formation flying with adaptive network topology B Shasti, A Alasty, N Assadian Acta Astronautica 136, 281-296, 2017 | 36 | 2017 |
| Soft landing on an irregular shape asteroid using multiple-horizon multiple-model predictive control MA AlandiHallaj, N Assadian Acta Astronautica 140, 225-234, 2017 | 33 | 2017 |
| On the quasi-equilibria of the BiElliptic four-body problem with non-coplanar motion of primaries N Assadian, SH Pourtakdoust Acta Astronautica 66 (1-2), 45-58, 2010 | 31 | 2010 |
| Prescribed-time control for perturbed Euler-Lagrange systems with obstacle avoidance A Shakouri, N Assadian IEEE Transactions on Automatic Control 67 (7), 3754-3761, 2021 | 29 | 2021 |
| Predictive fault-tolerant control of an all-thruster satellite in 6-DOF motion via neural network model updating MM Tavakoli, N Assadian Advances in Space Research 61 (6), 1588-1599, 2018 | 29 | 2018 |
| Optimal station-keeping near Earth–Moon collinear libration points using continuous and impulsive maneuvers M Ghorbani, N Assadian Advances in Space Research 52 (12), 2067-2079, 2013 | 28 | 2013 |
| Model predictive orbit control of a low earth orbit satellite using Gauss’s variational equations MM Tavakoli, N Assadian Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2014 | 24 | 2014 |
| Sliding mode control of electromagnetic tethered satellite formation MAA Hallaj, N Assadian Advances in space research 58 (4), 619-634, 2016 | 22 | 2016 |
| Multiple-horizon multiple-model predictive control of electromagnetic tethered satellite system MA AlandiHallaj, N Assadian Acta Astronautica 157, 250-262, 2019 | 21 | 2019 |
| Tethered satellite system control using electromagnetic forces and reaction wheels MAA Hallaj, N Assadian Acta Astronautica 117, 390-401, 2015 | 21 | 2015 |
| Integrated magnetometer–horizon sensor low-earth orbit determination using UKF M Farahanifar, N Assadian Acta Astronautica 106, 13-23, 2015 | 21 | 2015 |
| Geography of the rotational resonances and their stability in the ellipsoidal full two body problem MJ Nadoushan, N Assadian Icarus 265, 175-186, 2016 | 19 | 2016 |
| Prescribed-time control with linear decay for nonlinear systems A Shakouri, N Assadian IEEE Control Systems Letters 6, 313-318, 2021 | 18 | 2021 |
| Fault detection and isolation of satellite gyroscopes using relative positions in formation flying A Shakouri, N Assadian Aerospace Science and Technology 78, 403-417, 2018 | 17 | 2018 |
| Asteroid precision landing via probabilistic multiple-horizon multiple-model predictive control MA AlandiHallaj, N Assadian Acta Astronautica 161, 531-541, 2019 | 15 | 2019 |
| Stabilizing chaotic system on periodic orbits using multi-interval and modern optimal control strategies M Abedini, R Vatankhah, N Assadian Communications in Nonlinear Science and Numerical Simulation 17 (10), 3832-3842, 2012 | 14 | 2012 |
