Y. H. Fan, P. P. Yan, F. Yang, Hong Yang Xu, “Discrete Sliding Mode Control For Hypersonic Cruise Missile”, Discrete Dynamics In Nature And Society, 2016.
 Y. Hu, Z. Xiao, J. Li, “Missile PID Controller Parameter Tuning based on Iterative Learning Control”, 2nd International Conference on Signal Processing Systems, pp V3-689-692, 5-7 July 2010.
 C. Yuan, Y. Liu, F. Wu, C. Duan, “Hybrid Switched Gain-Scheduling Control for Missile Autopilot Design”, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 10, October 2016.
 Y. Lee, Y. Kim, G. Moon, B.-E. Jun, “Sliding-Mode-Based Missile-Integrated Attitude Control Schemes Considering Velocity Change”, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 3, January 2016.
 Chen Xianxiang, “Robust Gain-Scheduled Autopilot Design with LPV Reference Model for Portable Missile”, 2012 IEEE Aerospace Conference, pp. 1-10, 3-10 March 2012.
 U. Sefastsson, “Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model”, 2016.
 D.-Y. Won, M.-J. Tahk, K.-Y. Kim, “Robust Gain-Scheduling Technique for an Agile Missile Subject to Mass Variation”, ICCAS 2010, pp. 2119-2123, 27-30 October 2010.
 J. Lijin, T.J.S. Jothi, “Aerodynamic characteristics of an Ogive-Nose Spinning Projectile”, Sādhanā, Vol. 43, No. 4, April 2018.
 Y. Yun, J. Guo, S. Tang, “Robust Smooth Sliding-Mode-Based Controller with Fixed-Time Convergence for Missiles Considering Aerodynamic Uncertainty”, International Journal of Aerospace Engineering, 2018.
 R.E. Ak, M.R. Prasetyo, Z. Hidayat, “Designing an Optimal Control LQT for Controlling and Guidance of Missile”, Journal On Advanced Research In Electrical Engineering, Vol. 2, No. 1, April 2018.
 C.-H. Lee, B.-E. Jun, J.-Ik Lee, “Connections between Linear and Nonlinear Missile Autopilots via Three-Loop Topology”, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 6, January 2016.
 Z. Shi, F. Wang, X.-Z. Wang, “Design of Missile Lateral Channel Controller Based on QFT”, International Conference on Computational and Information Sciences, pp. 917-920, 21-23 Oct. 2011.
 S. Zhu, Z. Chen, H. Zhang, Z. Huang, H. Zhang, "Investigations on The Influence of Control Devices to the Separation Characteristics of a Missile From the Internal Weapons Bay", Journal of Mechanical Science And Technology, Vol. 32, No. 5, May 2018.
 Z. Shi, W. Ma, Y. Zhang, H. Han, “Lateral Thrust and Aerodynamics Compound Control System of Missile based on Adaptive Fuzzy Control “, 5th International Symposium on Computational Intelligence and Design, pp. 231-234, 28-29 Oct. 2012.
 H. Mahdianfar, E. Prempain, “Adaptive Augmenting Control Design for a Generic Longitudinal Missile Autopilot”, 2016 American Control Conference (ACC), pp. 3138-3143, 6-8 July 2016.
 O. Ognjanović, S. Maksimović, N. Vidanović, G. Kastratović, K. Maksimović, “Structural Analyses of Ballistic Missile Fin Configuration During Supersonic Flight Conditions”, International Journal of Engineering, Vol. 16, No. 1, February 2018.
 F.-K. Yeh, J.-J. Huang, C.-W. Huang” Integrated Design of Ballistic Missile Guidance and Autopilot using Adaptive Sliding Control with 5 DOF Inputs”, SICE Annual Conference, pp. 639-644, 13-18 September 2011.
 F.-K Yeh, “Adaptive-Sliding-Mode Guidance Law Design for Missiles with Thrust Vector Control and Divert Control System”, IET Control Theory & Applications, Vol. 6, No. 4, March 2012.
 H. Malek, M.M. Ebadzadeh, M. Rahmati, “Three New Fuzzy Neural Networks Learning Algorithms based on Clustering, Training Error and Genetic Algorithm”, Applied Intelligence, Vol. 37, No. 2, September 2012.
 B.-G. Park, H.-H. Kwon, Y.-H. Kim, “Composite Guidance Scheme for Impact Angle Control Against a Nonmaneuvering Moving Target”, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 5, January 2016.
 C. Dongyang, L.K. Abbas, R. Xiaoting, W. Guoping, “Aerodynamic and Static Aeroelastic Computations of a Slender Rocket with All-Movable Canard Surface”, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 232, No. 6, June 2017.
 S. He, J. Wang, D. Lin, “Robust Missile Autopilots With Finite-Time Convergence”, Asian Journal of Control, Vol. 18, No. 3, May 2016.
 B. Bangian Tabrizi, S.K. Hosseini Sani, “Control of Cruise STT Missile based on Dynamic Inversion using Genetic Algorithm and Neural Network and Virtual Boundary Layer Using Simulated Annealing Optimization”, 22nd Iranian Conference of Electrical Engineering, May 2014.