Feshe, W., Automated Rendezvous and Docking of Spacecraft,Cambridge University Press, 2003.
 Lee, D., Guidance, Navigation And Control Systems for Autonomous Proximity Operations and Docking of Spacecraft, Dissertation for the degree of Doctor of Philosophy in aerospace engineering, Missouri University of Science and technology, 2009.
 Yazhong, L., Jin, Zh. and Guojin, T., “Survey of orbital dynamics and control of space rendezvous,” Chinese Journal of Aeronautics, Vol. 27, 2014, pp. 1-11.
 Aldrin, J. E., Line-of-Sight Guidance Techniques for Manned Orbital Rendezvous, Dissertation for doctor of science, Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1963.
 Zhang, G. and Zhou, D., “An improved two-maneuver method for orbit rendezvous with constant thrust,” Proc. IMECHE, Part G: J. Aerospace Engineering, Vol. 226, 2012, pp. 1583-1592.
 Kasaeian, S. A., Assadian, N. and Ebrahimi, M., “Sliding mode predictive guidance for terminal rendezvous in eccentric orbits,” ELSEVIER, Acta Astronautica, Vol. 140, 2017, pp. 142-155.
 Wiesel, W. E. Space flight Dynamics, McGraw-Hill. Inc., 1989.
 Guglieri, G., Maroglio, F., Pellegrino, P. and Torre, L., “Design and development of guidance navigation and control algorithms for spacecraft rendezvous and docking experimentation,” Elsevier, Acta Astronautica, Vol. 94, 2014, pp. 395-408.
 Wu, S., Zhou, W. Y., Tan, S. J. and Wu, G. Q., “Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target,” Hindawi Publication Corporation, The Scientific World Journal, 2013, doi:10.1155/2013/579703.
 Yongqiang, Q, Yingmin, J. and Jian, W., “Robust control for constant thrust rendezvous under thrust failure,” Chinese Journal of Aeronautics, Vol. 28, 2015, pp. 518-526.
 Chiou, J.C., Hwang, M.C., Wuf, S.D. and Yang, J.Y., “Robust attitude control of spacecraft using sliding mode control and productive network,” International Journal of Systems Science, Vol. 28, 1997, pp. 435-446.
 Stott, JR. J.E., Classical and Higher-Order Sliding Mode Attitude Control for Launch Vehicle Systems, Dissertation for the degree of Doctor of Philosophy in the department electrical and computer engineering, The university of Alabama in Huntsville, 2009.
 Alikhani, A. and Kasaeian, S.A., “Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle,” Journal of Space science and technology (JSST), Vol. 8, Winter 2016, pp. 1-7.
 Tournes, C. and Shtessel, Y., “Automatic Docking Using Second Order Sliding Mode Control0,” Proceeding of the American Control Conference,New York City, 2007.
 Lian, Y. and Tang, G., “Libration point orbit rendezvous using PWPF modulated terminal sliding mode control,” ELSEVIER, Advances in Space Research, Vol. 52, 2013, pp. 2156-2167.
 Binglong, Ch. and Yunhai, G., “Super twisting controller for on-orbit servicing to non-cooperative target,” Chinese Journal of Aeronautics, Vol. 28, 2015, pp. 285-293.
 Vallado, D. A., Fundamentals of Astrodynamics and Applications, The McGraw-Hill Companies, Inc., College Custom Series, 1997.
 Tewari, A., Atmospheric and Space Flight Dynamics, Birkhauser, 2007.
 Wei, L., Yunhai, G., Xueqin, C. and Fan Z., “Relative Position and Attitude Coupled Control for Autonomous Docking with a Tumbling Target,” International Journal of Control and Automation, Vol. 4., No. 4, 2011.
 Wang, Y., Feng, Y. and Yu, X., “High-order Nonsingular Terminal Sliding Mode Control of Uncertain Multivariable Systems,” The 33rd Annual Conference of the IEEE Electronics Society (IECON), Taipei, Taiwan, 2007.
 Romdhane, N.M.B. and Damak, T., “Terminal sliding mode feedback linearization control,” International Journal of Sciences and Techniques of Automatic Control & Computer Engineering, Vol. 4, 2010, pp. 1174-1178.
 Liu, K., Liu, F., Wang, S. and Li, Y., “Finite-Time Spacecraft's Soft Landing on Asteroids Using PD and Nonsingular Terminal Sliding Mode Control,” Hindawi Publication Corporation, Mathematical Problems in Engineering, 2015.
 Harl, N. and Balakrishnan, S.N., “Reentry Terminal Guidance Through Sliding Mode Control,” Journal of Guidance, Control, and Dynamics,Vol. 33, 2010, pp. 186-199.