[1] Vijaya, M. S., Piezoelectric Materials and Devices: Applications in Engineering and Medical Sciences, Taylor and Francis Group, 2013.
[2] Koofigar, H. R., “Robust active vibration control of flexible beams in smart structures using piezoelectric sensors and actuators”, the Research Plan, No. 89001149, Isfahan University, 2012.
[3] Song, G., B. Kotejoshyer. “Vibration reduction of flexible structures during slew operations.” International Journal of Acoustics and Vibration, Vol.7, No.2, 2002, pp. 105-109.
[4] Shan, J. J., H. T. Liu, D. Sun. “Slewing and vibration control of a single-link flexible manipulator by positive position feedback.” Mechatronics, Vol. 15, No. 4, 2005, pp. 487-503.
[5] Jiang, J. P., D. X. Li. “Robust H∞ vibration control for smart solar array structure.” Journal of Vibration and Control, Vol.17, No.4, 2010, pp.505-515.
[6] Khoshnood, A., H. Moradi Maryamnegari. “Dynamics modeling and active vibration control of a satellite with flexible solar panels.” Modares Mechanical Engineering, Vol. 14, No.16, 2015, pp. 57-66 (in Persian).
[7] Marinaki, M., Y. Marinakis, G. E. Stravroulakis. “Vibration control of beams with piezoelectric sensors and actuators using particle swarm optimization.” Expert system Applied, Vol. 38, 2011, pp. 6872-6883.
[8] Song, G., B. N. Agrewal. “Vibration suppression of flexible spacecraft during attitude control.” Acta Astronautica, Vol. 49, No. 2, 2001, pp.73-83.
[9] Xiaoping, S., Y. Guopiang. “Robust attitude tracking control scheme for flexible spacecraft with vibration suspention”, 25th Chinese Control and Decision Conference, 2013.
[10] Ding, S., W. X. Zheng. “Non smooth attitude stabilization of a flexible spacecraft.” IEEE Transactions on Aerospace and Electronic Systems, Vol. 50, No. 2, 2014, pp. 1163-1183.
[11] Azadi, M., S. A. Fazelzadeh, M. Eghtesad, E. Azadi. “Vibration suppression of smart nonlinear flexible appendages of a rotating Satelite by using hybrid adaptive sliding mode / lyapunov control.” Journal of Vibration Control, 2013.
[12] Azadi, M., S. A. Fazelzadeh, M. Eghtesad, E. Azadi. “Active vibration suppression and maneuver control of an orbiting smart flexible satellite.” IJST, Transaction of Mechanical Engineering, Vol. 38 (M1), 2014, pp. 119-133.
[13] Sayanjali, M., J. Roshanian, A. Ghaafari. “Three axis maneuver of elastic spacecraft consist active vibration control.” Journal of Space Science and Technology, No.3, pp.43, 2009 (in Persian).
[14] Hu, Q. “Sliding mode attitude control with L2-gain performance and vibration reduction of flexible spacecraft with actuator dynamics.” Acta Astronautica, Vol. 67, 2010, pp. 572-583.
[15] Hu, Q., G. Ma. “Variable Structure Control and Active Vibration Suppression of Flexible Spacecraft during Attitude Maneuver.” Aerospace Science and Technology, Vol. 9, 2005, pp. 307-317.
[16] Meirovitch, L. Principles and Techniques of Vibrations, Prentice-Hall International, 1997.
[17] Slotine, J. J., W. Li. Applied Nonlinear Control, Prentice-Hall International, 1992.
[18] Malekzadeh, M., A. Naghash, H. A.Talebi. “Control of Flexible Spacecraft Using Dynamic Inversion and µ-Synthesis.” Journal of Vibration and Control, Vol. 17, No. 11, 2011.
[19] Zhou, K., and J. C. Doyle. Essentials of Robust Control, Prentice-Hall, 1998.