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  • Piramoon, S., Ayoubi, M. A., Bashash, S., “Modeling and Vibration Suppression of Rotating Machines Using the Sparse Identification of Nonlinear Dynamics and Terminal Sliding Mode Control,” IEEE Access, vol. 12, pp. 119272-119291, 2024, doi:10.1109/ACCESS.2024. 3449913.
  • Piramoon, S.; Ayoubi, M. A., “Neural-Network-Based Active Vibration Control of Rotary Machines,” IEEE Access, Vol. 12, pp. 107552–107569, 2024, https://doi.org/10.1109/ ACCESS.2024.3418981.
  •  Khanesar, M.A.; Yan, M.; Isa, M.; Piano, S.; Ayoubi, M. A.; Branson, D.T., “Enhancing Positional Accuracy of the XY-Linear Stage Using Laser Tracker Feedback and IT2FLS,” Machines 2023, 11, 497. https://doi.org/10.3390/machines11040497.

  • Hart, S. T., Ayoubi, M. A., and Naseradinmousavi, P., "Comparative Study of Pseudospectral Methods for Spacecraft Optimal Attitude Maneuvers", Journal of Spacecraft and Rockets, https://doi.org/10.2514/1.A35081.

  • Ayoubi, M. A. and Hsin J., "Sun-Avoidance Slew Planning with Keep-Out Cone and Actuator Constraints," Journal of Spacecraft and Rockets, Vol. 57, No. 6, pp. 1175-1185,
  • Margolis, B. W. L., and Ayoubi, M. A., Joshi, S. S., “Nonlinear Model Predictive Control of Reentry Vehicles Based on Takagi-Sugeno Fuzzy Models,” The Journal of Astronautical Sciences, 2019, doi:10.1007/s40295-019-00191-2.
  • Mazmanyan, L. and Ayoubi, M. A., “Fuzzy Attitude Control of Spacecraft with Fuel Sloshing via Linear Matrix Inequalities,” IEEE Transactions on Aerospace and Electronic Systems, 2018; doi: 10.1109/TAES.2018.2820419
  • Sendi, C. and Ayoubi, M. A., “Robust Fuzzy Tracking Control of Flexible Spacecraft via T-S Fuzzy Model,” IEEE Transactions on Aerospace and Electronic Systems, 2018; Vol (54), Issue 1, pp. 170–179. doi:10.1109/TAES.2017.2740078.
  • Baculi, J. and Ayoubi, M. A., “Fuzzy attitude control of solar sail via linear matrix inequalities”, Acta Astronautica, Vol.138, No. 9, pp. 233–241, https://doi.org/10.1016/j.actaastro.2017.05.021
  • Naseradinmousavi, P., Ghanipoor Machiani, S., Ayoubi, M. A., and Nataraj, C., "Coupled Operational Optimization of Smart Valve System Subject to Different Approach Angles of a Pipe Contraction", Journal of Structural and Multidisciplinary Optimization, doi: 10.1007/s00158-016-1554-7.
  • Sendi, C. and Ayoubi, M. A., “Robust-Optimal Fuzzy Model-Based Control of Flexible Spacecraft with Actuator Constraints”, Journal of Dynamic Systems, Measurement, and Control, Vol.138, No. 9, doi: 10.1115/1.4033318.
  • Ayoubi, M. A. and Sendi, C., “Takagi-Sugeno Fuzzy Model-Based Control of Spacecraft With Flexible Appendage”, Journal of Astronautical Sciences, DOI:10.1007/s40295-015-0035-3.
  • Ayoubi, M. A., Martin, K. M., Longuski, J. M., “Analytical Solution of the Motion for Spinning Thrusting Spacecraft with Transverse Ramp-Up Torques,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 4, 2014, pp. 1272—1282, DOI:10.2514/1.62695.
  • Ting, E. and Ayoubi, M. A. “Optimized Fuzzy Proportional/ Integral/ Derivative Controller for Aircraft Pitch Control,” Journal of Aerospace Information Systems, Vol. 10, No. 8, 2013, pp. 414—429.
  • Ayoubi, M. A., Goodarzi, F. A., and Banerjee, A., “Attitude Motion of a Spinning Spacecraft With Fuel Sloshing and Nutation Damping,” Journal of Astronautical Sciences, Vol. 58, No. 4, October–December 2011, pp. 551–568.
  • Ayoubi, M. A. and Tai, L.C., "Intelligent Control of a Large-Scale Variable Speed Wind Turbine," ASME Journal of Solar Energy Engineering, Vol. 134, No. 1, 2012.
  • Ayoubi, M. A. and Longuski, J. M., “Asymptotic Theory for Thrusting, Spinning-Up Spacecraft Maneuvers,” Acta Astronautica, Vol. 64, Issue 7, 2009, pp. 810-831.
  • Ayoubi, M. A. and Longuski, J. M., “Asymptotic Theory of Spinning Rigid Bodies Subject to Constant Forces.” Journal of Guidance, Control, and Dynamics, Vol. 31, No. 5, 2007, pp. 1511-1516.
  • Ayoubi, M. A. and Longuski, J. M., “Analytical Solutions for Translational Motion of Spinning-Up Rigid Bodies Subject to Constant Body-Fixed Moments and Forces,” ASME Journal of Applied Mechanics, Vol. 75, No.1, 2008.
  • Ayoubi, M. A. and Longuski, J. M., “Axial Velocity Solutions for Spinning-Up Rigid Body Subject To Constant Forces,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 6, 2007, pp. 1610-1619.
  • Longuski, J. M., Gick, R. A., Ayoubi, M. A., and Randall, L. “Analytical Solutions for Thrusting, Spinning Spacecraft Subject to Constant Forces,” Journal of Guidance, Control, and Dynamics, Vol.28, No. 6, 2005, pp. 1301-1309.

Peer-Reviewed Conference Papers:

  • Howard, A. and Ayoubi, M. A., “A Hybrid Data-Driven Approach for Autonomous Fault Detection and Prognosis of a Spacecraft Reaction Wheel,” AIAA Aviation Forum and ASCEND co-located Conference Proceedings, 2024, https://doi.org/10.2514/6. 2024-4807.
  • Si, Y. and Ayoubi, M. A., “Attitude Tracking Control of Spacecraft with Reaction Wheel Disturbances via Takagi-Sugeno Fuzzy Model,” presented at the 2022 AIAA SciTech Forum on January 3–7, 2022.
  • Hakim, V. and Ayoubi, M. A., "Optimal Steering of Nonredundant Single-Gimbal CMGs Using Gauss Pseudospectral Method," ID: 2576, to be presented at the 2021 IEEE Aerospace Conference on March 6--13, 2021.
  • Piramoon, S. and Ayoubi, M. A., "An Eigensystem Realization Algorithm for Modal Parameter Identification of a Vertical-Shaft High-Speed Centrifugal Machine," IMECE 2020-23087, presented at the 2020 International Mechanical Engineering Congress & Exposition (IMECE) on November 16--19, 2020.
  • Ayoubi, M. A. and Hsin J., “Sun-Avoidance Slew Planning Algorithm with Pointing and Actuator Constraints,” AAS 19-801, Presented at the 2019 AAS/AIAA Astrodynamics Specialist Conference, Portland, ME, August 11–15, 2019.
  • Ayoubi, M. A. and Peiman Naseradinmousavi, “Open-Loop Minimum-Energy Maneuver of a Solar-Sail Using Magnetic Torques and Reaction Wheels,” DSCC2018-9093, ASME Dynamic Systems and Control Conference, Atlanta, Georgia, Sept 30–Oct 3, 2018.
  • Mazmanyan, L. and Ayoubi, M. A., “Robust-Optimal Rule-Based Attitude Control of Spacecraft with Partially-Filled Fuel Tanks,” AAS 18-469, AAS/AIAA Astrodynamics Specialist Conference, Snowbird, Utah, August 19–23, 2018.
  • Margolis, Benjamin W. L., and Ayoubi, M. A., “Comparative Study of Tracking Controllers applied to Martian Aerocapture,” presented at the 2017 AAS/AIAA Astrodynamics Specialist Conference, Columbia River Gorge, Stevenson, WA, August 20–24, 2017.
  • Swei, Sean S. M. and Ayoubi, M. A., “LMI-Based Fuzzy Optimal Variance Control of Airfoil Model Subject to Input Constraints,” presented at the 2017 IEEE International Conference on Fuzzy Systems, Naples, Italy, July 9-12, 2017.
  • Baculi, J. and Ayoubi, M. A., “Fuzzy-Logic Supervisory Attitude Control of Solar Sail,” presented at the AIAA Space Conference, AIAA-2016-5646, Long Beach, California, September 13-16, 2016.
  • Baculi, J. and Ayoubi, M. A., “Fuzzy Attitude Control of Solar Sail with Translating Control Masses via Linear Matrix Inequalities,” presented at the 26th AAS/AIAA Space Flight Mechanics Meeting, AAS paper16-337, Napa, California, February 14-16, 2016.
  • Margolis, B. and Ayoubi, M. A., “Model Predictive Control of Planetary Aerocapture Using Takagi-Sugeno Fuzzy Model,” presented at the 26th AAS/AIAA Space Flight Mechanics Meeting, AAS paper16-407, Napa, California, February 14-16, 2016.
  • Swei, S., Ayoubi, M. A., and Nguyen, N. "Fuzzy Model-Based Optimal Covariance Control of Flexible Aircraft with Actuator Amplitude and Rate Constraints," presented at the AIAA SciTech Conference, San Diego, CA, January 4-8, 2016.
  • Sendi, C. and Ayoubi, M. A., “Robust-Optimal Fuzzy Model-Based Control of Flexible Spacecraft With Actuator Amplitude and Rate Constraints,” presented at the ASME Dynamic Systems and Control Conference, Columbus, OH, October 28-30, 2015.
  • Johnson, M. and Ayoubi, M. A., “Shared Fuzzy Control of Multiple Quadrotor UAVs With Time-Dependent Delay and Bounded Control-Input Constraint,” presented at the ASME Dynamic Systems and Control Conference, Columbus, OH, October 28-30, 2015.
  • Sendi, C. and Ayoubi, M. A., "Robust Fuzzy-Logic Based Control of Flexible Spacecraft with H_infinity  Performance Criteria," presented at the AIAA/AAS Astrodynamics Specialist Conference, San Diego California, August 4-7, 2014.
  • Mazmanyan, L. and Ayoubi, M. A., "Takagi-Sugeno Fuzzy Model-Based Attitude Control of Spacecraft with Partially-Filled Fuel Tanks," presented at the AIAA/AAS Astrodynamics Specialist Conference, San Diego California, August 4-7, 2014.
  • Ayoubi, M. A., Swei, S., and Nguyen, N. "Fuzzy Model-Based Stabilization and Vibration Suppression of Flexible Aircraft," presented at the American Control Conference, Portland, OR, June 4-6, 2014.
  • Ayoubi, M. A., Sendi, C., "Fuzzy-Logic Attitude Control of Spacecraft With Retargeting Flexible Antenna," AIAA Guidance, Navigation, and Control Conference, Boston, Massachusetts, August 19–22, 2013; doi:10.2514/6.2013-4861.
  • Mazmanyan, L., Ayoubi, M. A., "Attitude Motion of a Spinning Spacecraft With Fuel Sloshing in High-G Maneuvers," AAS 13-060, presented at the AAS/AIAA Astrodynamics Specialist Conference, Hilton Head, South Carolina, August 11–15, 2013.
  • Ayoubi, M. A. and Sendi, C., "Lyapunov-Based Attitude Tracking Control of a Quadrotor UAV, "Proceedings of ASME International Mechanical Engineering Congress and Exposition, Vol. 4, parts A and B, pp. 213-221, 2012;doi: 10.1115/IMECE2012-89517.
  •  Ayoubi, M. A. and Gazorpak, M., "Time-Optimal Attitude Control of a Quadrotor UAV, "Proceedings of ASME 2012 5th Annual Dynamic Systems and Control Conference Joint with the JSME 2012 11th Motion and Vibration Conference, DSCC 2012-MOVIC 2012, Vol. 3, pp. 73-79, 2012.
  • Ayoubi, M. A., Martin, K. M., Longuski, J. M. "Analytical Solution of the Motion of Spinning Thrusting Spacecraft with Transverse Ramp-Up Torques," AIAA/AAS Astrodynamics Specialist Conference, Minneapolis, Minnesota, August 13–16, 2012; doi:10.2514/6.2012-5015.
  • Ting, E. and Ayoubi, M. A., "An Optimal Fuzzy-PID Controller for Aircraft Pitch Control," AIAA Infotech @ Aerospace Conference, Garden Grove, California, June 19–21, 2012; doi: 10.2514/6.2012-2580.
  • Ayoubi, M. A., Landau, D., and Longuski, J. M., "Solution of Spacecraft Attitude Via Angular Momentum in Body and Inertial Frames," Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference, Vol. 142, pp. 2611-2628, 2012.
  • Ayoubi, M. A., Goodarzi, F. A., and Banerjee, A., "Attitude Motion of a Spinning Spacecraft with Fuel Sloshing and Nutation Damping," Advances in the Astronautical Sciences: Proceedings of the 21st AAS/AIAA Space Flight Mechanics Meeting, Vol. 140, pp. 97-109, 2011.
  • Ayoubi, M. A. and Tai, L. C., "Adaptive Neuro-Fuzzy Control of a Wind Turbine Operating in Region 3," Proceedings of ASME 2010 International Mechanical Engineering Congress and Exposition, Vol. 8: Dynamic Systems and Control, Parts A and B, Vancouver, British Columbia, Canada, November 12–18, 2010; doi: 10.1115/IMECE2010-40970.
  • Ayoubi, M. A. and Longuski, J. M., "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, Vol. 2, pp. 1468-1479, 2006.
  • Medlock, K. Gates, Ayoubi, M. A., and Longuski, J. M., "Analytic Solutions for Aerocapture, Descent, and Landing Trajectories for Dual-Use Ballute Systems," Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, Vol. 1, pp. 147-171, 2006.
  • Ayoubi, M. A. and Longuski, J. M., "Transverse Velocity Solution for a Spinning-Up Rigid Body Subject To Constant Body-Fixed Moments and Forces," Advances in the Astronautical Sciences - Proceedings of the AAS/AIAA Astrodynamics Conference, Vol. 123 I, pp. 183-197, 2006.
  • Krozel, J., Andrisani II, D., Ayoubi, M. A., and Hoshizaki, T., "ADS-B Data Integrity Check, "Collection of Technical Papers - AIAA 4th Aviation Technology, Integration, and Operations Forum, ATIO, Vol. 1, pp. 231-241, 2004.
  • Malaek, M.B., and Ayoubi, M. A., Optimal Control of Commercial Airplane Landing Distance, proceedings of the ISME (Iranian Society of Mechanical Engineers) Conference, Sharif University of Technology, Tehran, Iran, Vol. 1, 2000, pp. 391–398.
  • Nakhaie, G.R., and Ayoubi, M. A., Satellite Orbit Perturbation Due to Oblate Earth Gravitational Field, proceedings of the ISME Conference, Sharif University of Technology, Tehran, Iran, Vol. 2, 1994, pp. 168–176
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Associate Professor of Mechanical Engineering

Email: maayoubi@scu.edu

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