[1] Zarchan, P., Tactical and Strategic Missile Guidance, AIAA, 2002, pp Reston.
[2] Nathan, H., Balakrishnan, S.N. and Craig, P., “Sliding Mode Integrated Missile Guidance and Control,” AIAA Guidance, Navigation, and Control Conference, Toronto, Ontario Canada, August 2010.
[3] Shkolnikov, I., Shtessel, Y. and Lianos, D., “Integrated Guidance-Control System of a Homing InterceptorSliding Mode Approach,” Presented as Paper AIAA, 2001-4218 at the AIAA Guidance, Navigation, and Control Conference and Exhibit, August, 2001.
[4] Shtessel, Y. and Buffington, J., “Continuous Sliding Mode Control,” Proceedings of the American Control Conference, 1998.
[5] Brown, M., Shtessel, Y. and Buffington, J., “Finite Reaching Time Continuous Sliding Mode Control with Enhanced Robustness,” Proceedings of the AIAA Guidance, Navigation, and Control Conference, Denver, CO, August, 2000.
[6] Shtessel, Y., Shkolnikov, I. and Brown, M., “An Asymptotic Second Order Smooth Sliding Mode Control,” Asian Journal of Control, Vol. 5, No. 4, 2003, pp. 498 – 504.
[7] Shtessel, Y. and Shkolnikov, I., “Integrated Guidance and Control of Advanced Interceptors using Second Order Sliding Modes,” Proceedings of the 42nd IEEE Conference on Decision and Control, 2003.
[8] Shtessel, Y., Shkolnikov, I. and Levant, A., “Guidance and Control of Missile Interceptor using Second-Order Sliding Modes,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 45, No. 1, 2009, pp. 110-124.
[9] Shtessel, Y. and Tournes, C., “Integrated Higher-Order Sliding Mode Guidance and Autopilot for Dual-Control Missiles,” Journal of Guidance, Control, and Dynamics, Vol. 32, No. 1, 2009.
[10] Shima, T., Idan, M. and Golan, O., “Sliding-Mode Control for Integrated Missile Autopilot Guidance,” Presented as Paper AIAA-2004-4884 at the AIAA Guidance, Navigation, and Control Conference and Exhibit, August 2004.
[11] Chen, H., Dong, C. and Wang, Q., “Integrated Guidance and Control Backstepping Design Based on Integral Sliding Mode Surface for Missiles,” Presented as Paper 33rd Chinese Control Conference, July, Nanjing, China, 2014.
[12] Mohammadzaman, I. and Momeni, H.R., “Short Time Stability Approach to Guidance Law Design,” Journal of Space Science and Technology, Vol. 3, No.2, 2010, pp. 37-44 (In Persian).
[13] Slotine, J. J. E. and Li, W., Applied Nonlinear Control, Prentice–Hall, Upper Saddle River, NJ, 1991, pp. 276–309.
[14] Khalil, H. K., Nonlinear Systems, 3rd edition [M], New Jersey, Prentice-Hall, Chap 4, 2002.
[15] Moon, J., and Kim, Y., “Design of Missile Guidance Law Via Variable Structure Control,” Proceedings of AIAA Guidance, Navigation and Control Conference, Denver, CO, 2000, Paper AIAA-2000-4068.
[16] Hong, Y.G., “Finite Time Stabilization and Stabilizability of a Class of Controllable Systems,” Systems & Control Letters, Vol. 46, No. 4, 2002, pp. 231–236.
[17] Shtessel, Y., Shkolnikov, I., and Brown, M., “An Asymptotic Second Order Smooth Sliding Mode Control,” Asian Journal of Control, Vol. 5, No. 4, 2003, pp. 498 – 504.
[18] Shtessel, Y. and Shkolnikov, I., “Integrated Guidance and Control of Advanced Interceptors using Second Order Sliding Modes.” Proceedings of the 42nd IEEE Conference on Decision and Control, December, 2003.
[19] Shtessel, Y., Shkolnikov, I., and Levant, A., “Guidance and Control of Missile Interceptor using Second-Order Sliding Modes,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 45, No. 1, 2009, pp. 110-124.
[20] Shtessel, Y. and Tournes, C., “Integrated Higher-Order Sliding Mode Guidance and Autopilot for Dual-Control Missiles,” Journal of Guidance, Control, and Dynamics, Vol. 32, No. 1, 2009, pp. 79-94
[21] Shima, T., Idan, M. and Golan, O., “Sliding-Mode Control for Integrated Missile Autopilot Guidance,” Presented as Paper AIAA-2004-4884 at the AIAA Guidance, Navigation, and Control Conference and Exhibit, August 2004.
[22] Chen, H., Dong, C. and Wang, Q., “Integrated Guidance and Control Backstepping Design Based on Integral Sliding Mode Surface for Missiles,” Presented as Paper 33rd Chinese Control Conference, Nanjing, China, July 2014.
[23] Mohammadzaman, I. and Momeni, H.R., “Short Time Stability Approach to Guidance Law Design,” Journal of Space Science and Technology, Vol. 3, No.2, 2010, pp. 37, 44 (In Persian).
[24] Slotine, J. J. E. and Li, W., Applied Nonlinear Control, Prentice–Hall, Upper Saddle River, NJ, 1991, pp. 276–309.
[25] Khalil, H. K., Nonlinear Systems, 3rd edition [M], New Jersey, Prentice-Hall, Chap 4, 2002.
[26] Moon, J. and Kim, Y.,“Design of missile guidance law via variable structure Control,” Proceedings of AIAA Guidance, Navigation and Control Conference, Denver, CO, 2000, Paper AIAA-2000-4068.
[27] Hong, Y.G., “Finite Time Stabilization and Stabilizability of a Class of Controllable Systems,” Systems & Control Letters, Vol. 46, No. 4, 2002, pp. 231–236.
[28] Qian, C., Lin, W., “Non-Lipshchitz Continues Stabilizer Fornonlinear Systems with Uncontrollable Unstable Linearization,” System and Control Letters, Vol. 42, Issue 3, 2001, pp.185-200.
[29] Ozgoli. S. and Arvan, M.R., Modeling and Simulation of Moving Systems, Ya Mahdi Publication, 2010 (In Persian).
[30] Arvan, M.R., Modeling of Electro-Optical Seeker and Line of Sight Rate Estimation in the Presence of Disturbances, (PhD Thesis), KN Toosi University, 2006 (In Persian).
[31] Arora, V.K., Former Director Defence Science Centre Delhi, Proximity Fuzes Theory and Techniques, Defence Research and Development Organization Ministry of Defence NEwDELm-110 105 2010.
[32] Siouris, G. M., Missile Guidance and Control Systems, Springer-Verlog Publisher, 2004.
[33] Kahveckuglu, A.,Tool for Designing Robust Autopilot for Ramjet Missiles, (M. Sc. Thesis), The Graduate School of Natural and Applied Sciences of The Middle East Technical University, 2006.
[34] Theodoulis, S. and Duc, G., “Missile Autopilot Design Gain Scheduling and the Gap Metric,” Journal of Guidance, Control and Dynamics, Vol. 32, No. 3, 2002, pp. 986 -996.
[35] Mingzhe, H., Xiaoling, L. and Guangren
, D.,“Adaptive Block Dynamic Surface Control for Integrated Missile Guidance and Autopilot,”
Chinese Journal of Aeronautics, Vol. 26, Issue 3, 2013, Pages 741-750.
[36] Fridman, L., Iriarte, R. and Moreno, J., Sliding Modes after the First Decade of the 21st Century, Springer-Verlag Berlin Heidelberg, 2011.
[37] Eker, I., “Sliding mode control with PID Sliding Surface and Experimental Application to an Electromechanical Plant,”ISA Transactions, Vol. 45, Issue 1, 2006, pp. 109–118.
[38] Rubagotti, M., Estrada,
A., Castanos,
F., Ferrara,
A. and Fridman,
L., “Integral Sliding Mode Control for Nonlinear Systems With Matched and Unmatched Perturbations,”
IEEE Transactions on Automatic Control, Vol. 56, Issue 11, 2011, pp. 2699 – 2704.