| Modeling and control of fuel cell using artificial neural networks HSA Al-Amir, HA Dahd, EAE Sheet Journal of Engineering 21 (12), 124-138, 2015 | 10 | 2015 |
| Overcome uncertainties of vertical take-off and landing aircraft based on optimal sliding mode control WS Aboud, HSA Al-Amir, AA Alhamdany, FM Kadhim Indones. J. Electr. Eng. Comput. Sci 29, 703-714, 2023 | 2 | 2023 |
| Vibration control of clamped affected by dynamic load with electromagnetic actuator SH Abiduan, HS Abd Al-Amir, WS Aboud Association of Arab Universities Journal of Engineering Sciences 25 (1), 170-182, 2018 | 1 | 2018 |
| Influence of Flap Angle on the Aeroelastic Behavior of Wing-Flap Configuration Using Fully Coupled Structure-Fluid Interaction Model MA Tawfik, MI Abu-Tabikh, HS Abd Al-Amir Eng. & Tech. Journal 29 (7), 2011 | 1 | 2011 |
| Flutter Estimation for Low Speed Aircraft Wing Using Fully Coupled Fluid–Structure Interaction MA Tewfik, MI Abu-Tabikh, HS Abd Al-Amir Engineering & Technology Journal 31, 0 | 1 | |
| A Robust Controller Design for Simple Robotic Human Arm WS Aboud, HK Aljobouri, HS Abd Al-Amir Indonesian Journal of Electrical Engineering and Informatics (IJEEI) 10 (3 …, 2022 | | 2022 |
| NONLINEAR NEURAL PID CONTROLLER FOR DEPRESSING FLUCTUATION OF CURVED BEAM SUBJECTED TO DIFFERENT LOAD CONDITIONS WS ABOUD, HS ABD AL-AMIR, HS JABER Journal of Engineering Science and Technology 17 (4), 2431-2446, 2022 | | 2022 |
| A STUDY OF A TRANSMITTED FORCE FROM HARMONIC MOVING LOAD ON A BEAM SUPPORTED BY NONLINEAR VIBRATION ISOLATOR HS Abd Al-Amir Journal of Techniques 29 (1), 2016 | | 2016 |
| On line auto-tuning robust nonlinear neural PID controller design for double –pipe heat exchanger based on particle swarm optimization HSA Al-Amir Al-Rafidain University College For Sciences 7, 2016 | | 2016 |
| Modeling and nonlinear control of overhead crane based on moving load concept HSA Al-Amir Journal of the Federation of Arab Universities for Engineering Studies and …, 2015 | | 2015 |
| Flutter Condition Estimation for 3-D Cantilever Plate Using Fully Coupled fluid – Structure Interaction HSAAA Dr. Mauwafak A. Tawfik, Dr. Mohammed I. Mohsin Eng. &Tech. Journal 32 (12), 2014 | | 2014 |
| Flutter Estimation for Low Speed Aircraft Wing Using Fully Coupled Fluid–Structure Interaction HS Abd Al-Amir, MI Abu-Tabikh, MA Tewfik Engineering and Technology Journal 31 (16 Part (A) Engineering), 2013 | | 2013 |
| Control on 3-D Fixable Wing Flutter Using an Adaptive Neural Controller MA Tawfik, MI Abu-Tabikh, HS Abd Al-Amir Engineering and Technology Journal 30 (16), 2012 | | 2012 |
| Control on a 2-D Wing Flutter Using an Adaptive Nonlinear Neural Controller MA Tawfik, MI Mohsin, HS Abd Al-Amir Al-Khwarizmi Engineering Journal 7 (4), 27-40, 2011 | | 2011 |
