Crouch, P., Spacecraft attitude control and stabilization: Applications of geometric control theory torigid body models, IEEE Transactions on Automatic Control, vol.29, no.4, 1984, pp.321-331.
[2] Singh, S.N. and Iyer, A., Nonlinear decoupling sliding mode control and attitude control of spacecraft, IEEE Transactions on Aerospace and Electronic Systems, vol.25, no.5, pp.621-633, 1989.
[3]Wei B. and Barba,P. M., Quaternion Feedback for Spacecraft Large Angle Maneuvers, J.Guid. Contr. Dynam.,vol. 8, no. 3, 1985, pp. 360-365.
[4]Wallsgrove, R.J. and Akella, M.R., Globally stabilizing saturated attitude control in the presence ofbounded unknown disturbances, Journal of Guidance, Control and Dynamics, vol.28, no.5, 2005, pp.957-963.
[5] Cai, W.C., Liao, X.H. and Song, Y.D., Indirect robust adaptive fault-tolerant control for attitudetracking of spacecraft, Journal of Guidance, Control and Dynamics, vol.31, no.5, 2008, pp.1465-1463.
[6] Seo, D. and Akella, M.R., Separation property for the rigid-body attitude tracking control problem, Journal of Guidance, Control and Dynamics, vol.30, no.6, 2007, pp.1569-1576.
[7] Song, Y.D. and Cai, W.C., Quaternion observer-based model-independent tracking control of spacecraft, Journal of Guidance, Control and Dynamics, vol. 32, no.5, 2009, pp.1476-1482.
[8] Park, Y., Inverse optimal and robust nonlinear attitude control of rigidspacecraft, Aerospace Science and Technology, 2012. http://dx.doi.org/ 10.1016/j.ast.2012.11.006.
[9] Su, Y. and Zheng, C., Simplenonlinear proportional-derivative control for globalfinite- time stabilization of spacecraft, Journal of Guidance, Control and Dynamics, vol. 38, no.1, 2015
[10]Juang, J.C., Jan, Y.W. and Lin, C.T., quaternion feedback attitude control design, A nonlinear H∞ approach, Asian Journal of Control, vol. 5, no. 3, pp. 406-411, 2003.
[11]Kristiansen, R., Nicklasson, P.J. and Gravdahl J.T., Satellite attitude control by quaternion-based back stepping, IEEE Trans. Control Systems Technology, vol. 17, no. 1, 2009, pp. 277-283.
[12]Zou, A.M., Kumar, K. D. and Hou, Z. G., Quaternion-based adaptive output feedback attitude control of spacecraft using Chebyshev neural networks, IEEE Trans. Neural Networks, vol.21, no. 9, pp.1457-1462, 2010.
[13] Alipour, M.R., FaniSaberi, F. and Kabganian, M., Modelling, design andexperimental implementation of non-linear attitude tracking with disturbance compensation using adaptive-sliding control based on quaternion algebra, The Aeronautical Journal, vol. 122, 2018, pp. 148-171,.
[14] Ma, Y. Jiang, B., Tao, G. and Cheng, Y., Actuator failure compensation and attitude control for rigid satellite by adaptive control using quaternion feedback, Journal of Francklin Institude, vol. 351, 2014, pp.296-314.
[15] Song, C., Kim, S.J. and Kim, S.H., Robust control of the missile attitude based on quaternion feedback, Control Engineering Practice, vol. 14, 2006, pp. 811–818.
[16] Xia, Y., Lu, K., Zhu, Z. and Fu, M., Adaptive back-stepping sliding mode attitude control of missile systems Int. J. Robust. Nonlinear Control, 2013.DOI: 10.1002/rnc.2952
[17]Hoseini S.M., Farrokhi M., and Koshkouei, A.J., Robust adaptive control of nonlinear non-minimum phase systems with uncertainties, Automatica, vol. 47, 2011, pp. 348–357.
[18]Jie, G., Yongzhi, S. and Xiangdong, L., Finite-time sliding mode attitude control for a reentry vehicle with blended aerodynamic surfacesand a reaction control system, Chinese, Journal of Aeronautics, vol. 27, no.4, 2014, pp. 964–976.
[19]Song, Y.D. and Cai W.C., New Intermediate quaternion based control of spacecraft: part I-almost global attitude tracking, International Journal of Innovative Computing, Information and Control, vol. 8, no. 10, 2012.
[20] Hall, J. S., Analysis and experimentation of control strategies for underactuated spacecraft, Ph.D. dissertation, Dept. Mech. and Astro. Eng., Naval Postgraduate School, Monterey, CA, 2009.
[21] Hoseini, S. M., Farrokhi, M., and Koshkouei, A. J. "Adaptive neural network output feedback stabilization of nonlinear non-minimum phase systems", Int. J. Adapt. Control Signal Process, vol. 24, 2010, pp. 65-82.
[22] Hoseini, S. M., Havaii, M., Amelian, J. and Shahmirzai, M., Robust adaptive control of flexible manipulators using multilayer percepron, J. Intell. Fuzzy Systems.
[23] Farmanbordar, A., and Hoseini, S. M., "Neural network adaptive output feedback control of flexiblelink manipulators," J. Dyn. Sys., Meas., Control, vol. 135, no. 2, 2012.
[24] Titterton, D. H. Strapdown Inertial Navigation Technology, American Institute of Aeronautics and Astronautics lnc, 2004.