Xinsan, L.I., Lixin, W. and Xiaohu, F. Two-stage control guidance of missile impact angle and flight time, Journal of National University of Defense Technology, 2017, 39, (6), pp 6–11.
Erer, K.S. and Tekin, R. Impact time and angle control based on constrained optimal solutions, Journal of Guidance, Control and Dynamics, 2016, 39, (10), pp 1–7.
Taub, I. and Shima, T. Intercept angle missile guidance under time varying acceleration bounds, Journal of Guidance, Control and Dynamics, 2013, 36, (3), pp 686–699.
Lee, C.H., Kim, T.H. and Tahk, M.J. Interception angle control guidance using proportional navigation with error feedback, Journal of Guidance, Control and Dynamics, 2013, 36, (5), pp 1556–1561.
Wang, H., Lin, D. and CHENG, Z. Optimal guidance of extended ballistic shaping, Chinese Journal of Aeronautics, 2014, 27, (5), pp 1259–1272.
Wang, X., Wang, Z. and LIN, H. A cooperative guidance law with constraints of impact time and impact angle, Journal of Ballistics, 2017, 29, (4), pp 1–8.
Zhang, X., Liu, M. and LI, Y. Backstepping sliding mode control and extended state observer based guidance law design with angles, Systems Engineering and Electronics, 2017, 39, (6), pp 1311–1316.
Wang, X. and Hong, Y. Finite-time consensus for multi-agent networks with second-order agent dynamics, IFAC Proceedings Volumes, 2018, 41, (2), pp 15185–15190.
Xiong, S., Wang, W. and Wang, S. Nonsingular fast terminal sliding-mode guidance with intercept angle constraint, Control Theory & Applications, 2014, 31, (3), pp 269–278.
Zhao, B., Zhou, J. and Lu, X. Adaptive integral sliding mode guidance law considering impact angel constraint, Control and Decision, 2017, 32, (11), pp 1966–1972.
Zhao, Y., Li, P. and Liu, J. Finite-ime sliding mode control based 3D guidance law with impact angle constraints, Journal of Beijing University of Aero- nautics and Astronautics, 2018, 44, (2), pp 273–279.
Si, Y. and Song, S. Design of three-dimensional finite-time guidance law for intercepting hypersonic vehicle, Journal of Chinese Inertial Technology, 2017, 25, (3), pp 405–414.
Arie, L. Principles of 2-sliding mode design, Automatica, 2007, 43, (4), pp 576–586.
Sun, L.H., Wang, W.H. and YI, R. A novel guidance law using fast terminal sliding mode control with impact angle constraints, ISA Transactions, 2016, 64, pp 12–23.
Peng, L., Xuefeng, P., Jianjun, M. and Shuai, T Non-homogeneous disturbance observer–based second order sliding mode control for a tailless aircraft, Proceedings of Chinese Automation Congress, 2013, pp 120–125. doi: 10.1109/cac.2013.6775713.
Kumar, S.R. Nonsgular terminal sliding mode guidance with impact angle constraints, Journal of Guidance, Control, and Dynamics, 2014, 37, (4), pp 1114–1130.
Zhang, Y. Finite-time convergent guidance law with impact angle constraint based on sliding-mode control, Nonlinear Dynamics, 2012, 70, (1), pp 619–625.
Bhat, S.P. and Bernstein, D.S. Finite-time stability of continuous autonomous systems, SIAM Journal on Control and Optimization, 2000, 38, (3), pp 751–766.
Lee, Y. and Kim, Y. Three-dimensional impact angle control guidance law for missiles using dual sliding surfaces, IFAC Proceedings Volumes, 2013, 46, (19), pp 137–142.
Zhou, H. Study on guidance law and cooperative guidance for multi-missiles based on finite–time and sliding mode theory, Harbin Institute of Technology, 2015, pp 41–44.