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References

1 
P. Zarchan, Tactical & Strategic Missile Guidance, AIAA, pp. 13-34, 2012.URL
2 
S. Jeong, Sungjin Cho, E. Kim, “Angle Constraint Biased PNG,” 2004 5th Asian Control Conference, pp. 1849-1854, 2004.URL
3 
C Chawla, P Sarmah, and R Padhi, “Suboptimal reentry guidance of a reusable launch vehicle using pitch plane maneuver,” Aerospace Science Technology, vol. 14, no. 16, pp. 377-386, 2010.DOI
4 
Ebrahimia, B., Bahrami, M., and Roshanianc, J. “Optimal sliding-mode guidance with terminal velocity constraint for fixed-interval propulsive maneuvers,” Acta Astronautica, vol. 62, no. 10-11, pp. 556-562, 2008.DOI
5 
H. Cho, and C.K. Ryoo, “Closed-Form Optimal Guidance Law for Missiles of Time-Varying Velocity,” Journal of Guidance, Control, and Dynamics, vol. 19, no. 5, pp. 1017-1022, 1996.DOI
6 
Yeh, F., Chien, H., and Fu, L. “Design of Optimal Midcourse Guidance Sliding-Mode Control for Missiles with TVC,” IEEE Trans. Aerosp. Electron. Syst. vol. 39, pp. 824-837, 2003.DOI
7 
Sungjin Cho, “Analytic Solution for Nonlinear Impact-Angle Guidance Law with Time-Varying Thrust,” Mathematics, vol. 10, no. 4034, pp. 1-13, 2022.DOI
8 
Defu Lin1, Yi Ji1, Wei Wang, Yuchen Wang, Hui Wang, and Fubiao Zhang, “Three-dimensional impact angle-constrained adaptive guidance law considering autopilot lag and input saturation,” International Journal of Robust and Nonlinear Control, vol. 10, no. 9, pp. 3653-3671, 2020DOI
9 
Sungjin Cho, “Autopilot Performance Analysis for Nonlinear Impact Angle Guidance Law with Time-Varying Thrust,” Korean Society of Aeronautical and Space Science 2023 Spring Conference, pp. 262-263, 2023.URL