| Year |
Citation |
Score |
| 2019 |
Margolis BWL, Ayoubi MA, Joshi SS. Nonlinear Model Predictive Control of Reentry Vehicles Based on Takagi-Sugeno Fuzzy Models The Journal of the Astronautical Sciences. 67: 113-136. DOI: 10.1007/S40295-019-00191-2 |
0.354 |
|
| 2017 |
Baculi J, Ayoubi MA. Fuzzy attitude control of solar sail via linear matrix inequalities Acta Astronautica. 138: 233-241. DOI: 10.1016/J.Actaastro.2017.05.021 |
0.312 |
|
| 2016 |
Sendi C, Ayoubi MA. Robust-Optimal Fuzzy Model-Based Control of Flexible Spacecraft With Actuator Constraint Journal of Dynamic Systems, Measurement and Control, Transactions of the Asme. 138. DOI: 10.1115/1.4033318 |
0.307 |
|
| 2016 |
Naseradinmousavi P, Machiani SG, Ayoubi MA, Nataraj C. Coupled operational optimization of smart valve system subject to different approach angles of a pipe contraction Structural and Multidisciplinary Optimization. 1-15. DOI: 10.1007/S00158-016-1554-7 |
0.307 |
|
| 2014 |
Ayoubi MA, Martin KM, Longuski JM. Analytical solution for spinning thrusting spacecraft with transverse Ramp-Up torques Journal of Guidance, Control, and Dynamics. 37: 1272-1282. DOI: 10.2514/1.62695 |
0.727 |
|
| 2014 |
Mazmanyan L, Ayoubi MA. Attitude motion of a spinning spacecraft with fuel sloshing in high-g maneuvers Advances in the Astronautical Sciences. 150: 793-812. |
0.369 |
|
| 2013 |
Ayoubi MA, Sendi C. Takagi-Sugeno fuzzy model-based control of spacecraft with flexible appendage Aiaa Guidance, Navigation, and Control (Gnc) Conference. DOI: 10.1007/S40295-015-0035-3 |
0.344 |
|
| 2012 |
Ayoubi MA, Martin KM, Longuski JM. Analytical solution of the motion of spinning thrusting spacecraft with transverse ramp-up torques Aiaa/Aas Astrodynamics Specialist Conference 2012. DOI: 10.2514/6.2012-5015 |
0.676 |
|
| 2012 |
Ayoubi MA, Landau D, Longuski JM. Solution of spacecraft attitude via angular momentum in body and inertial frames Advances in the Astronautical Sciences. 142: 2611-2628. |
0.692 |
|
| 2011 |
Ayoubi MA, Goodarzi FA, Banerjee A. Attitude motion of a spinning spacecraft with fuel sloshing and nutation damping Advances in the Astronautical Sciences. 140: 97-109. DOI: 10.1007/Bf03321531 |
0.548 |
|
| 2009 |
Ayoubi MA, Longuski JM. Asymptotic theory for thrusting, spinning-up spacecraft maneuvers Acta Astronautica. 64: 810-831. DOI: 10.1016/J.Actaastro.2008.12.015 |
0.72 |
|
| 2008 |
Ayoubi MA, Longuski JM. Asymptotic theory and limiting cases for spinning spacecraft subject to constant forces Q Journal of Guidance, Control, and Dynamics. 31: 1511-1515. DOI: 10.2514/1.35602 |
0.695 |
|
| 2008 |
Ayoubi MA, Longuski JM. Analytical solutions for translational motion of spinning-up rigid bodies subject to constant body-fixed forces and moments Journal of Applied Mechanics, Transactions Asme. 75: 0110041-0110048. DOI: 10.1115/1.2755110 |
0.747 |
|
| 2007 |
Ayoubi MA, Longuski JM. Axial velocity solution for spinning-up rigid bodies subject to constant forces Journal of Guidance, Control, and Dynamics. 30: 1610-1618. DOI: 10.2514/1.29617 |
0.735 |
|
| 2006 |
Ayoubi MA, Longuski JM. Axial velocity solution for a spinning-up rigid body subject to constant body-fixed forces and moments Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 2: 1468-1479. |
0.724 |
|
| 2006 |
Medlock KLG, Ayoubi MA, Longuski JM, Lyons DT. Analytic solutions for aerocapture, descent, and landing trajectories for dual-use ballute systems Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 1: 147-171. |
0.523 |
|
| 2006 |
Ayoubi MA, Longuski JM. Transverse velocity solution for a spinning-up rigid body subject to constant body-fixed forces and moments Advances in the Astronautical Sciences. 123: 183-197. |
0.739 |
|
| 2005 |
Longuski JM, Gick RA, Ayoubi MA, Randall L. Analytical solutions for thrusting, spinning spacecraft subject to constant forces Journal of Guidance, Control, and Dynamics. 28: 1301-1308. DOI: 10.2514/1.12272 |
0.737 |
|
| Show low-probability matches. |