Mohammad A. Ayoubi, Ph.D.
Affiliations: | 2006 | Aeronautics and Astronautics | Purdue University, West Lafayette, IN, United States |
Area:
Aerospace Engineering, Applied Mechanics, Mechanical EngineeringGoogle:
"Mohammad Ayoubi"Mean distance: (not calculated yet)
Parents
Sign in to add mentorJames M. Longuski | grad student | 2006 | Purdue | |
(Analytical theory for the motion of spinning rigid bodies.) |
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Publications
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Margolis BWL, Ayoubi MA, Joshi SS. (2019) Nonlinear Model Predictive Control of Reentry Vehicles Based on Takagi-Sugeno Fuzzy Models The Journal of the Astronautical Sciences. 67: 113-136 |
Baculi J, Ayoubi MA. (2017) Fuzzy attitude control of solar sail via linear matrix inequalities Acta Astronautica. 138: 233-241 |
Sendi C, Ayoubi MA. (2016) Robust-Optimal Fuzzy Model-Based Control of Flexible Spacecraft With Actuator Constraint Journal of Dynamic Systems, Measurement and Control, Transactions of the Asme. 138 |
Naseradinmousavi P, Machiani SG, Ayoubi MA, et al. (2016) Coupled operational optimization of smart valve system subject to different approach angles of a pipe contraction Structural and Multidisciplinary Optimization. 1-15 |
Ayoubi MA, Martin KM, Longuski JM. (2014) Analytical solution for spinning thrusting spacecraft with transverse Ramp-Up torques Journal of Guidance, Control, and Dynamics. 37: 1272-1282 |
Mazmanyan L, Ayoubi MA. (2014) Attitude motion of a spinning spacecraft with fuel sloshing in high-g maneuvers Advances in the Astronautical Sciences. 150: 793-812 |
Ayoubi MA, Sendi C. (2013) Takagi-Sugeno fuzzy model-based control of spacecraft with flexible appendage Aiaa Guidance, Navigation, and Control (Gnc) Conference |
Ayoubi MA, Martin KM, Longuski JM. (2012) Analytical solution of the motion of spinning thrusting spacecraft with transverse ramp-up torques Aiaa/Aas Astrodynamics Specialist Conference 2012 |
Ayoubi MA, Landau D, Longuski JM. (2012) Solution of spacecraft attitude via angular momentum in body and inertial frames Advances in the Astronautical Sciences. 142: 2611-2628 |
Ayoubi MA, Goodarzi FA, Banerjee A. (2011) Attitude motion of a spinning spacecraft with fuel sloshing and nutation damping Advances in the Astronautical Sciences. 140: 97-109 |