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References

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2 
L. Kim, H. Sung, Y. Jeon, S. Cho, 2012, Numerical study on flow characteristics of a variable thrust side jet thruster with a rectangular nozzle, The Korean Society of Propulsion Engineers Conf., pp. 110-116Google Search
3 
P. Zarchan, 2012, Tactical & Strategic Missile Guidance, 6th ed., Reston, VA: AIAAGoogle Search
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S. Kumar, D. Ghose, 2015, Impact time guidance for large heading errors using sliding mode control, IEEE trans. Aerospace and Electronic Systems, vol. 51, Vol. no. 5, No. pp. 3123-3138, pp. octoberDOI
5 
M. Tahk, C. Ryoo, H. Cho, 2002, Recursive time- to-go estimation for homing guidance missiles, IEEE trans. Aerospace and Electronic Systems, vol. 38, Vol. no. 1, No. pp. 13-24, pp. januaryDOI
6 
B. Park, 2014, Composite Guidance Law for Impact Angle Control of Passive Homing Missiles, Journal of the Korean Society for Aeronautical & Space Sciences, vol. 42, Vol. no. 1, No. pp. 20-28, pp. januaryDOI
7 
S. Cho, 2021, Dual Mode Guidance Algorithm for Initial Heading Error, The Korean Society of Aeronautical Science Conf., pp. 1-2Google Search