[1] M. Navabi, S. Soleymanpour, Standard and robust backstepping control of a spacecraft with inertial uncertainty (revision), Modares Mechanical Engineering, Vol. 14, No. 16, pp. 112-124, 2015. (in Persian فارسی )
[2] M. Navabi, M. Tavana, H. Mirzaei, Attitude control of spacecraft by state dependent riccati equation and power series expansion of riccati methods, Space Science and Technology, Vol. 7, No. 4, pp. 39-49, 2015. (in Persian فارسی )
[3] A. Iyer , S. N. Singh, Minimal realizations from MFDs and attitude control of spinning satellite using gyrotorquers, Proceedings of The 26th Institute of Electrical and Electronics Engineers Conference on Decision and Control, Los Angeles, United States of America, pp. 1269-1274, December 9-11, 1987.
[4] Y. P. Chen, S. C. Lo, Sliding-Mode controller design for spacecraft attitude tracking maneuvers, Institute of Electrical and Electronics Engineers Transactions on Aerospace and Electronic Systems, Vol. 29, No. 4, pp. 1328-1333, 1993.
[5] J. J. E. Slotine, W. Li, Applied Nonlinear Control, pp. 207-271, New Jersey: Prentice-Hall, 1991.
[6] Y. N. Fei, Q. H. Wu, Tracking control of robot manipulators via output feedback linearization, Frontiers of Mechanical Engineering in China, Vol. 1, No. 3, pp. 329-335, 2006.
[7] S. John, J. O. Pedro, Hybrid feedback linearization slip control for anti-lock braking system, Acta Polytechnica Hungarica, Vol. 10, No. 1, pp. 81-99, 2013.
[8] Y. Long, S. Lyttle, N. Pagano, D. J. Cappelleri, Design and quaternion-based attitude control of the omnicopter MAV using feedback linearization, Proceedings of The American Society of Mechanical Engineers International Design Engineering Technical Conference, Chicago, United States of America, August 12-15, 2012.
[9] H. Bang, J. S. Lee, Y. J. Eun, Nonlinear attitude control for a rigid spacecraft by feedback linearization, Mechanical Science and Technology, Vol. 18, No. 2, pp. 203-210, 2004.
[10] M. Navabi, N. Nasiri, Modeling and simulating the earth magnetic field utilizing the 10th generation of IGRF and comparison the linear and nonlinear transformation in order to use in satellite attitude control, Space Science and Technology, Vol. 3, No. 4, pp. 45-52, 2011. (in Persian فارسی )
[11] I. Kök, Comparison and Analysis of Attitude Control Systems of a Satellite Using Reaction Wheel Actuators, Master Thesis, Department of Computer Science Electrical and Space Engineering, Luleå University of Technology, Sweden, 2012.
[12] D. E. Kirk, Optimal Control Theory an Introduction, pp. 209-219, New York: Dover Publications, 2004.
[13] M. Navabi, H. R. Mirzaei, Dynamic modeling and nonlinear adaptive control of mesicopter flight, Modares Mechanical Engineering, Vol. 15, No. 5, pp. 1-12, 2015. (in Persian فارسی )
[14] J. Kim, J. Crassidis, A comparative study of sliding mode control and time-optimal control, Proceedings of The American Institute of Aeronautics and Astronautics/American Astronautical Society, Astrodynamics Specialist Conference and Exhibit, Boston, United States of America, August 10-12, 1998.
[15] M. J. Sidi, Spacecraft Dynamics and Control: A Practical Engineering Approach, pp. 95-169, New York: Cambridge university press, 1997.
[16] M. Navabi, N. Nasiri, Attitude control of microsatellite in terms of energy consumption for reaction wheel and magnetorquer actuators, Proceedings of The 10th Conference of Iranian Aerospace Society, Tehran, Iran, March 1-3, 2010. (in Persian فارسی )
[17] M. Rahmani, A. Ghanbari, Computed torque control of a caterpillar robot manipulator using neural network, Advanced Engineering Forum, Vol. 15, pp. 106-118, 2016.
[18] H. K. Khalil, Nonlinear Systems, Third Edittion, pp. 505-530, New Jersey: Prentice-Hall, 1996.
[19] M. Navabi, S. Soleymanpour, Command filtered modular adaptive backstepping attitude control of spacecraft in presence of disturbance torque, Modares Mechanical Engineering, Vol. 15, No. 7, pp. 285-296, 2015. (in Persian فارسی )
[20] B. S. Anjali, A. Vivek, J. L. Nandagopal, Simulation and analysis of integral LQR controller for inner control loop design of a fixed wing micro aerial vehicle (MAV), Procedia Technology, Vol. 25, pp. 76-83, 2016.
[21] Y. Yang, Analytic LQR design for spacecraft control system based on quaternion model, Aerospace Engineering, Vol. 25, No. 3, pp. 448-453, 2011.
[22] B. D. Anderson, J. B. Moore, Linear Optimal Control, pp. 70-77, New Jersey: Prentice-Hall, 1971.
[23] Z. Shulong, A. Honglei, Z. Daibing, A new feedback linearization lqr control for attitude of quadrotor, Proceedings of The 13th Institute of Electrical and Electronics Engineers International Conference on Control Automation Robotics & Vision, Marina Bay Sands, Singapore, pp. 1593-1597, December 10-12, 2014.