| Robust optimal solution for a smart rigid–flexible system control during multimode operational mission via actuators in combination M Azimi, S Moradi Multibody System Dynamics 52 (3), 313-337, 2021 | 16 | 2021 |
| Nonlinear dynamic and stability analysis of an edge cracked rotating flexible structure M Azimi, S Moradi International Journal of Structural Stability and Dynamics 21 (07), 2150091, 2021 | 12 | 2021 |
| Form-Finding and Free Vibration Analysis of a Class-One Triplex Tensegrity Prism M َAzimi, S Moradi Space Science and Technology 16 (3), 15-26, 2023 | | 2023 |
| ANALYTIC APPROXIMATE SOLUTION FOR NONLINEAR DYNAMICMODELING OF THE ROTATING ELASTIC 2D BEAM WITH A SINGLE CRACK AT Maleki, M Azimi, S Moradi Facta Universitatis, Series: Mechanical Engineering, 2022 | | 2022 |
| Active Vibration Control of a Maneuvering Flexible Spacecraft using Hybrid Actuators: A Lyapunov-Based Control Approach M َAzimi, S Moradi Space Science and Technology 15 (2), 1-14, 2022 | | 2022 |
| Dynamic and Stability Analysis of a Cracked Rotating Flexible Beam M َAzimi, S Moradi Space Science and Technology 14 (3), 51-63, 2021 | | 2021 |
| Vibration Suppression of a Maneuvering Flexible Spacecraft with Actuator Dynamic M Azimi, S Moradi Journal of Technology in Aerospace Engineering 5 (1), 45-56, 2021 | | 2021 |
| Application of Advanced Control Systems in Flexible Space Vehicles S Moradi Technology in Aerospace Engineering 3 (2), 41-51, 2019 | | 2019 |
Milad azimiKhayyam Research Institute (Ministry of Science, Research and Technology)Verified email at ari.ac.ir
