Luo W., Chu, Y. C., and Ling K.V., “Inverse Optimal Adaptive Control for Attitude Tracking of Spacecraft,” IEEE Transactions on Automatic Control, Vol. 50, No. 11, 2005, pp. 1639–1654.
 Slotine, J. J. E., and Li W.P., Applied Nonlinear Control, Upper Saddle River, NJ: Prentice-Hall, 1991.
 Behal, A., Dawson, D., Zergeroglu, E., and Fang, Y., “Nonlinear Trackingcontrol of an Underactuated Spacecraft,” J. Guid., Control Dyna., Vol. 25,No. 5, 2002, pp. 979–985.
 Boˇskovic´, J. D., Li, S.-M., and Mehra, R. K., “Robust Adaptive Variable Structure Control of Spacecraft under Input Saturation,” J. Guid., ControlDyna., Vol. 24, No.1, 2001, pp. 14–22.
 Boˇskovic´, J. D., Li, S.M., and Mehra, R. K., “Robust Tracking Control Design for Spacecraft under Control Input Saturation,”AIAA Journal of Guidance, Control & Dynamics, Vol.27, No.4, 2004, pp. 627-633.
 Xing, G. Q. and Parvez, A. S., “Nonlinear Attitude State Tracking Control for Spacecraft,” J. Guid., Control Dyna., Vol.24, No.3, 2001, pp. 624–626.
 Sharma, R. and Tewari, A., “Optimal Nonlinear Tracking of Spacecraft Attitude Maneuvers,” IEEE Trans. Control Syst. Technol., Vol. 12, No. 5, 2004, pp. 677–682.
 Krstic´, M., Kanellakopoulos, I. and Kokotovic, P., Nonlinear and Adaptive Control Design,New York: Wiley, 1995.
 Osborn, P. V., Whitaker, H. P. and Keezer, A, “New Developments in the Design of Adaptive Control Systems,”29th Annual Meeting ofthe Institute of Aeronautical Sciences, New York, No. 61-39, 1996.
 Popov, V. M., “Hyperstability of AUlOmatic Control Systems”, New York: Springer-Verlag, 1973.
 Thawar, T., “Adaptive Control of Rigid Body Satellite,”International Journal of Automation and Computing, Vol. 5, No. 3, 2008, pp. 296-306.
 Bolandi, H., Saberi, F., and Ghorbani, B, “Designof A Supervisory Adaptive Attitude Control (SAAC) System for A Stereo-Imaginary Satellite Based on Multiple Model Control With Switching,”International Journal of Innovative Computing, Information and Control, Vol. 6, No. 9, 2010, pp. 1–09-0365.
 Wertz, J. R., Spacecraft Attitude Determination and Control, D. Reidel, Dordrecht, New York, 1980.
 Van Den Bosch, P., Jongkind, W. and Swieten, A., “Adaptive Attitude Control for Large-angle Slew Maneuvers,” Automatica, Vol. 22, No. 2, 1986, pp. 209–215.
 Benchoubane, H., Stoten, D. P., “The Decentralized Minimal Controller Synthesis Algorithm,”International Journal of Control, Vol. 56, 1992, No. 4, pp. 967–983.
 Bolandi, H., Saberi, F., and Eslami,A, “Designof A Attitude Control System for A Satellite with accurate modeling of Reaction Wheels as actuators,”Journal of aerospace science and technology, No. 1, 2012, pp. 20.
 Shengmin, Ge., Hao, Ch., “A Comparative Design of Satellite Attitude Control System with Reaction Wheel,” Proceedings of the First NASA/ESA Conference on Adaptive Hardware and Systems, IEEE, 2006.
 Masteron, R.A., Miller, D.W. and Grogan, R.L., “Development and Validation of Reaction Wheel Disturbance Models: Empirical Model,” Journal of Sound and Vibration,Vol. 249, No. 3, 2002, pp. 575-598.
 Azarnoush, H., “Fault Diagnosis in Spacecraft Attitude Control System,”(M.S Thesis), Concordia University, Canada, 2005.