[1] R. H., Battin, An Introduction to the Mathematics and Methods Astrodynamics, Revised edition, Reston: AIAA Incc., 1999.
[2] M. A. Masoumnia, Q_Guidance in rotating coordinates, AIAA-01-2784-CP, 1991.
[3] S. Nelson, P. Zarchan, Alternative Approach to the solution of Lambert’s Problem, Journal of Guidance, control and dynamics, Vol.15, No.4, 1992.
[4] P. Zarchan, Tactical and Strategic Missile Guidance, Vol. 124, Progress in Astronautics and Aeronautics, AIAA , 1990.
[5] GH. Alizadeh, Guidance Algoritm for cut-off insensitive Balistic Missile, Thesis of PHD, Modares Universiry, 1378. (In Persian)
[6] M. R. Amini, Guidance Agoritm for Ballistic Missie, thesis of master of science, Tehran University, 1374. (In Persian)
[7] N. Prabhakar, I. D. Kumar, A Predictive Explicit Guidance Scheme for Ballistic Missile, Defence Science Journal, Vol. 6, No. 5, pp. 456-461, India, 2013.
[8] R. Esmaelizadeh, Functional Guidance Method for ballistic missie, Thesis of M.Sc., Amir Kabir University, 1379. (In Persian)
[9] S. M. Hoseini, Design and Simulation of Near Guidance System for Ballistic Missile, Thesis of Master of Sceience in Control Engineering, Iran University of Science and Tecnology, 2001.
[10] N. Gahremani, Predicted Guidance Method based on prediction of solid propellant burning time, Thesis of PHD Amir Kabir University, 1388.
[11] A. U. Ishlinski, Inertial guidance of Ballistic Missile, Moscow, 1968
[12] K. A. Hoffman, S. T. Chiang, Computational Fluid Dynamics Engineering, Volume one, 1993.
[13] R. L. Burden, J. D. Fairs, Numerical Analysis, 9th edition, 2010.
[14] M. Havaei, Guidance and Control Design of a short Range Aerodynamic Control Missile, Thesis of M.Sc., Tarbiat Modares University, Tehran, 1395. (In Persian)