| Aircraft ADS-B data integrity check J Krozel, D Andrisani, M Ayoubi, T Hoshizaki, C Schwalm AIAA 4th aviation technology, integration and operations (ATIO) Forum, 6263, 2004 | 50 | 2004 |
| Robust fuzzy tracking control of flexible spacecraft via a T–S fuzzy model C Sendi, MA Ayoubi IEEE Transactions on Aerospace and Electronic Systems 54 (1), 170-179, 2017 | 33 | 2017 |
| Fuzzy attitude control of spacecraft with fuel sloshing via linear matrix inequalities L Mazmanyan, MA Ayoubi IEEE Transactions on Aerospace and Electronic Systems 54 (5), 2526-2536, 2018 | 25 | 2018 |
| Analytical solutions for thrusting, spinning spacecraft subject to constant forces JM Longuski, RA Gick, MA Ayoubi, LA Randall Journal of Guidance, Control, and Dynamics 28 (6), 1301-1308, 2005 | 24 | 2005 |
| Intelligent control of a large variable speed wind turbine MA Ayoubi, LC Tai | 20 | 2012 |
| Asymptotic theory for thrusting, spinning-up spacecraft maneuvers MA Ayoubi, JM Longuski Acta Astronautica 64 (7-8), 810-831, 2009 | 19 | 2009 |
| Fuzzy attitude control of solar sail via linear matrix inequalities J Baculi, MA Ayoubi Acta Astronautica 138, 233-241, 2017 | 18 | 2017 |
| Robust Fuzzy Logic-Based Tracking Control of a Flexible Spacecraft with Performance Criteria C Sendi, MA Ayoubi AIAA SPACE 2014 Conference and Exposition, 4417, 2014 | 15 | 2014 |
| Takagi-sugeno fuzzy model-based attitude control of spacecraft with partially-filled fuel tank L Mazmanyan, MA Ayoubi AIAA/AAS astrodynamics specialist conference, 4215, 2014 | 15 | 2014 |
| Attitude motion of a spinning spacecraft with fuel sloshing and nutation damping MA Ayoubi, FA Goodarzi, A Banerjee The Journal of the Astronautical Sciences 58 (4), 551-568, 2011 | 14 | 2011 |
| Coupled operational optimization of smart valve system subject to different approach angles of a pipe contraction P Naseradinmousavi, SG Machiani, MA Ayoubi, C Nataraj Structural and Multidisciplinary Optimization 55, 1001-1015, 2017 | 13 | 2017 |
| Takagi-Sugeno fuzzy model-based control of spacecraft with flexible appendage MA Ayoubi, C Sendi The Journal of the Astronautical Sciences 61, 40-59, 2014 | 12 | 2014 |
| Optimized fuzzy-proportional/integral/derivative controller for aircraft pitch control E Ting, MA Ayoubi Journal of Aerospace Information Systems 10 (8), 414-429, 2013 | 12 | 2013 |
| Analytical solutions for translational motion of spinning-up rigid bodies subject to constant body-fixed forces and moments MA Ayoubi, JM Longuski | 12 | 2008 |
| Fuzzy model-based pitch stabilization and wing vibration suppression of flexible aircraft MA Ayoubi, SSM Swei, NT Nguyen 2014 American Control Conference, 3083-3088, 2014 | 10 | 2014 |
| Robust-optimal fuzzy model-based control of flexible spacecraft with actuator constraint C Sendi, MA Ayoubi Journal of Dynamic Systems, Measurement, and Control 138 (9), 091004, 2016 | 9 | 2016 |
| An optimal fuzzy-PID controller for aircraft pitch control E Ting, M Ayoubi Infotech@ Aerospace 2012, 2580, 2012 | 8 | 2012 |
| Robust-optimal fuzzy model-based control of flexible spacecraft with actuator amplitude and rate constraints C Sendi, MA Ayoubi Dynamic Systems and Control Conference 57243, V001T06A005, 2015 | 7 | 2015 |
| Analytical solution for spinning thrusting spacecraft with transverse ramp-up torques MA Ayoubi, KM Martin, JM Longuski Journal of Guidance, Control, and Dynamics 37 (4), 1272-1282, 2014 | 7 | 2014 |
| LMI-based fuzzy optimal variance control of airfoil model subject to input constraints SSM Swei, MA Ayoubi 2017 IEEE International Conference on Fuzzy Systems (FUZZ-IEEE), 1-6, 2017 | 6 | 2017 |
