[1] Zarchan, P., Tactical and Strategic Missile Guidance, AIAA Series, Vol. 199, 2002, pp. 143–152.
[2] Siouris, G. M., Missile Guidance and Control Systems, Springer, 2005, pp. 194–228.
[3] Behnamgol, V., Vali, A.R. and Mohammadi, A., “A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics,”
Journal of Space Science and Technology (JSST), Vol. 8, No. 4, Winter 2016, pp. 9-16.
[4] Behnamgol, V., Vali, A. R. and Mohammadi, A., “A New Observer-Based Chattering-Free Sliding Mode Guidance Law,” ProcIMechE Part G, J. Aerospace Engineering , Vol. 230, No.8, 2016, pp. 1486–1495.
[5] Zhou, D., Sun, Sh., Zhou, J.Y., Teo, K.L. “A Discrete Sliding-Mode Guidance Law,” Transactions of the ASME, Journal of Dynamic Systems, Measurement, and Control, Vol. 137, 2015, pp. 6
[6] Liu, L., Zhu, J., Tang, G. and Bao, W. “Diving guidance via feedback linearization and sliding mode control,” Aerospace Science and Technology, Vol. 41, 2015, pp. 16–23.
[7] Modirrousta, A., Sohrab, M. and Dehghan, S.M. “A modified guidance law for ground moving target tracking with a class of the fast adaptive second-order sliding mode,” SAGE Transactions of the Institute of Measurement and Control, 2015, pp.1–13.
[8] Shtessel, Y. B., Shkolnikov, I. A., and Levant, A., “Smooth second-order sliding modes: Missile guidance application,” Automatica, No. 43, 2007, pp. 1470 – 1476.
[9] Behnamgol, V., Mohammadzaman, I., Vali, A.R., Ghahramani. N.A., “Guidance Law Design using Finite Time Second Order Sliding Mode Control,” Journal of Control, K.N. Toosi University of Technology, Vol. 5, No. 3, 2011, pp. 36-45.
[10] Harl, N. and Balakrishnan, S. N., “Impact Time and Angle Guidance with Sliding Mode Control,” IEEE Transaction on Control Systems Technology, 2011.
[11] Ryoo, C., Cho, H., and Tahk, M., “Closed-Form solutions of optimal guidance with terminal impact angle constraint,” in Proc. IEEE Conf. Control Appl., 2003, pp. 504–509.
[12] Jeong, S., Cho, S., and Kim, E., “Angle constraint biased PNG,” in Proc. 5th Asian Control Conf., 2004, pp. 1849–1854.
[13] Lu, P., Doman, D., and Schierman, J., “Adaptive terminal guidance for hypervelocity impact in specified direction,” presented at the AIAA Guidance. Navigation. Control Conf. Exhibit, San Francisco, CA, 2005.
[14] Xu, Q., Yu, J., Yu, J., and Yang, X., “Integrated guidance/autopilot design for missiles with impact angle constraints,” in Proc. IEEE Int. Conf. Inform. Acquisition, 2006, pp. 75–79.
[15] Ryoo, C., Cho, H., and Tahk, M., “Time-to-Go weighted optimal guidance with impact angle constraints,” IEEE Trans. Control Syst. Technology., Vol. 14, No. 3, May 2006, pp. 483–492.
[16] Sang, D., Min, B., and Tahk, M., “Impact angle control guidance law using Lyapunov function and PSO method,” in Proc. Annu. SICE Conf., 2007, pp. 2253–2257.
[17] Ratnoo, A., and Ghose, D., “SDRE based guidance law for impact angle constrained trajectories,” presented at the AIAA Guid., Nav., Control Conf. Exhibit, Hilton Head, 2007.
[18] Rao, S., and Ghose, D., “Sliding Mode Control based Terminal Impact Angle Constrained Guidance Laws using Dual Sliding Surface”, 12th IEEE Workshop on Variable Structure Systems, January 12-14, Mumbai, 2012.
[19] Gu, W., Zhang, U., YU, J.,“A three-dimensional Missile Guidance Law with Angle Constraint Based on Sliding Mode Control”, 2007 IEEE International Conference on Control and Automation, Guangzhou, CHINA - May 30 to June 1, 2007.
[20] Komurcugil, H., “Adaptive terminal sliding-mode control strategy for DC–DC buck converters”, Elsevier ISA Transactions 51, 2012, pp. 673–681.
[21] Chiu, Ch. S., “Derivative and integral terminal sliding mode control for a class of MIMO nonlinear systems”, Elsevier Automatica, 48, 2012, pp. 316–326.
[22] Zhou, D., and Sun, S., “Guidance Laws with Finite Time Convergence,” Journal of Guidance, Control, and Dynamics, 32, pp. 1838-1846, 2009.
[23] Janardhanan, S., and Bandyopadhyay, B., "On Discretization of Continuous-TimeTerminal Sliding Mode", IEEE TRANSACTIONS ON AUTOMATIC CONTROL, VOL. 51, NO. 9, SEPTEMBER 2006, pp. 1532- 1536.
[24] Kumar, Sh. R., Rao, S., and Ghose, D., “Sliding Mode Guidance and Control for All Aspect interceptors with Terminal Angle Constraints”, Journal of Guidance, Control, and Dynamics, Vol. 35, No. 4, july – August 2012.
[25] Zhang, U., Sun, M., Chen, Z., “Finite-time convergent guidance law with impact angle constraint based on sliding-mode control”, Springer, Nonlinear Dynamics, Published online 07 June 2012.
[26] Behnamgol, V., Vali, A. R., Mohammadi, A., "Designing Guidance Law For Intercepting With Limited Angle Using Terminal Sliding Mode Control," 13th Conference of Iranian Aerospace Society, Tehran, IRAN, 23-25 February 2014.
[27] Feng, Y., Yub, X., Han, F., “On nonsingular terminal sliding-mode control of nonlinear systems”, Elsevier Automatica 49, 2013, pp. 1715–1722.
[28] Li, K., Cao, J., and Yu, F., “Study on the Nonsingular Problem of Fractional-Order Terminal Sliding Mode Control”, Hindawi Publishing Corporation, Mathematical Problems in Engineering, 2013.
[29] Kumar, Sh. R., Rao, S., and Ghose, D., “Non-singular Terminal Sliding Mode Guidance and Control with Terminal Angle Constraints for Non-maneuvering Targets”, 12th IEEE Workshop on Variable Structure Systems, January 12-14, Mumbai, 2012.
[30] Khalil, H. K., Nonlinear Systems, Prentice-Hall, Upper Saddle River, NJ, 1996, pp. 601-617.
[31] Slotine, J. J. E., and Li, W., Applied Nonlinear Control, Prentice-Hall, Upper Saddle River, NJ, 1991, pp. 276-309.
[32] Fridman, L., Moreno, J., and Iriarte, R., Sliding Modes after the First Decade of the 21st Century, Springer, 2011.
[33] Feng, Y., Yu, X., Man, Zh., “Non-singular terminal sliding mode control of rigid manipulators”, Elsevier, Automatica 38, 2002, pp. 2159 – 2167.
[34] Sun, Sh., Zhou, D., Hou, W., “A guidance law with finite time convergence accounting for autopilot lag”, Elsevier, Aerospace Science and Technology 25, 2013, pp. 132–137.
)