[10] [10] DOHRMANN C R, EISLER G R, ROBINETT R D. Dynamic programming approach for burnout-to-apogee guidance of precision munitions［J］. Journal of Guidance, Control, and Dynamics, 1996, 19(2): 340-346.

[11] [11] RAHIMI A, KUMAR K D, ALIGHANBARI H. Particle swarm optimization applied to spacecraft reentry trajectory［J］. Journal of Guidance, Control, and Dynamics, 2013, 36(1): 307-310.

[12] [12] ZHOU D, QU P P, SUN S. A guidance law with terminal impact angle constraint accounting for missile autopilot［J］. Journal of Dynamic Systems, Measurement, and Control, 2013, 135(5). doi: 10. 1115/1. 4024202.

[13] [13] RUSNAK I, WEISS H, ELIAV R, et al. Missile guidance with constrained intercept body angle［J］. IEEE Transac-tions on Aerospace and Electronic Systems, 2014, 50(2): 1145-1453.

[18] [18] BREDA D, MASET S, VERMIGLIO R. Pseudospectral methods for stability analysis of delayed dynamical systems［J］. International Journal of Dynamics and Control, 2014, 2(2): 143-153.