Zarchan P ， Tactical and strategic missile guidance, fifth edition (Progress in Astronautics and Aeronautics), AIAA, 5th ed., 2007.
 Siouris GM, Missile Guidance and Control Systems, Springer, New York, 2003.
 Oza HB and Padhi R, Impact-angle-constrained suboptimal model predictive static programming guidance of air-to-ground missiles, J Guidance Cont Dynam, Vol.35, No.1, 2012, pp. 153–164.
 Kim BS, Lee JG and Han SH, Biased PNG law for impact with angular constraint, IEEE Trans Aerosp Electron Syst, Vol.34, No.1, 1998, pp. 277–288.
 Erer KS and Merttopçuo LO, Indirect impactangle- control against stationary targets using biased pure proportional navigation, J Guidance Cont Dynam, Vol.35, No.2, 2012, pp. 700–703.
 Kim TH, Park BG and Tahk MJ, Bias-shaping method for biased proportional navigation with terminal-angle constraint, J Guidance Cont Dynam; Ahead of print: 1–6.
 Lu P, Doman DB and Schierman JD, Adaptive terminal guidance for hypervelocity impact in specified direction, J Guidance Cont Dynam, Vol.29, No.2, 2006, pp. 269-278.
 Ratnoo A and Ghose D, Impact angle constrained interception of stationary targets, J Guidance Cont Dynam, Vol.31, No.6, 2008, pp. 1816–1821.
 Lee YI, Kim SH and Tahk MJ, Optimality of linear time-varying guidance for impact angle control, IEEE Trans Aerosp Electron Syst, Vol.48, No.4, 2012, pp. 2802–2817.
 Dwivedi PN, Bhattacharya A and Padhi R, Computationally efficient suboptimal midcourse guidance using model predictive static programming, In: Proceedings of IFAC World Congress, Seoul, ROK, 6-11 July 2008, pp.3550-3555.
 Tatiya M, Bhatia N and Padhi R, Impact angle constrained suboptimal terminal guidance of interceptors for air defence, In: Proceedings of 18th IFAC Symposium on Automatic Control in Aerospace, Nara, Japan, 6-10 September 2010, pp.130-135.
 Ryoo CK, Cho H and Tahk MJ, Optimal guidance laws with terminal impact angle constraint, J Guidance Cont Dynam, Vol.28, No.4, 2005, pp. 724–732.
 Ryoo CK, Cho H and Tahk MJ, Time-to-go weighted optimal guidance with impact angle constraints, IEEE T Contr Syst T, Vol.14, No.3, 2006, pp. 483–492.
 Ratnoo A and Ghose D, Impact angle constrained guidance against nonstationary nonmaneuvering targets, J Guidance Cont Dynam, Vol.33, No.1, 2010, pp. 269–275.
 Turetsky V and Shinar J, Missile guidance laws based on pursuit-evasion game formulations, Automatica, Vol.39, No.4, 2003, pp. 607-618.
 Adler FP, Missile guidance by threedimensional proportional navigation, J Appl Phys, Vol.27, No.5, 1956, pp. 500-507.
 Xu XY and Cai YL, Optimal guidancelaw and control of impact angle for the Kinetic Kill Vehicle, Proc IMechE, Part G, Journal of Aerospace Engineering, Vol.225, No.9, 2011, pp. 1027~1036.
 Ben-Asher JZ and Yaesh I, Advances in Missile Guidance Theory, vol. 180, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 1998, pp. 25–90.
 Garber V, Optimum Intercept Laws for Accelerating Targets, AIAA Journal, Vol.6, No.11, 1968, pp. 2196–2198.