［5］ Zhou D, Mu C D, Xu W L. Adaptive sliding-mode guidance of a homing missile［J］. Journal of Guidance, Control, and Dynamics, 1999, 22(4): 589-584.
[2]
［6］ Moon J, Kim K, Kim Y. Design of missile guidance law via variable structure control［J］. Journal of Guidance, Control, and Dynamics, 2001, 24 (4): 659-664.
[3]
［7］ Rusnak I, Meir L. Optimal guidance for acceleration constrained missile and maneuvering target［J］. IEEE Transactions on Aerospace and Electronic Systems, 1990, 26(4): 618-624.
[4]
［8］ Rusnak I, Meir L. Optimal guidance for high order and acceleration constrained missile［J］. Journal of Guidance, Control, and Dynamics, 1991, 14(3): 589-596.
[5]
［13］ Farrell J, Sharma M, Polycarpou M. Backstepping-based flight control with adaptive function approximation［J］. Journal of Guidance, Control and Dynamics, 2005, 28(6): 1089-1101.
[6]
［14］ Sonneveldt L, Chu Q P, Mulder J A. Nonlinear flight control design using constrained adaptive backstepping［J］. Journal of Guidance, Control and Dynamics, 2007, 30(2): 322-336.
[7]
［15］ Chwa D, Choi J Y. Adaptive nonlinear guidance law considering control loop dynamics［J］. IEEE Transactions on Aerospace and Electronics Systems, 2003, 39(4): 1134-1143.
［19］ Liaw D C, Liang Y W, Cheng C C. Nonlinear control for missile terminal guidance［J］. Journal of Dynamic Systems, Measurement, and Control, 2000, 122: 663-668.
[12]
［20］ Shafiei M H, Binazadeh T. Partial stabilization-based guidance［J］ . ISA Transactions, 2012, 51(4): 141-145.
[13]
［21］ Shafiei M H, Binazadeh T. Application of partial sliding mode in guidance problem［J］. ISA Transactions, 2013, 52(2):192-197.
[14]
［1］ Zarchan P. Tactical and strategic missile guidance［M］. 3rd ed. Washington: American Institute of Aeronautics and Astronautics, 1997.
[15]
［9］ Rusnak I. Advanced guidance laws for acceleration constrained missile, randomly maneuvering target and noisy measurements［J］. IEEE Transactions on Aerospace and Electronic Systems, 1996, 32(1): 456-464.
[16]
［10］ Hexner G, Shima T, Weiss H. LQG guidance law with bounded acceleration command［J］. IEEE Transactions on Aerospace and Electronic System, 2008, 44(1): 77-86.
[17]
［11］ Hexner G, Pila A. W. Practical stochastic optimal guidance law for bounded acceleration missiles［J］. Journal of Guidance, Control, and Dynamics, 2011, 34(2): 437-445.
[18]
［12］ Farrell J, Polycarpou M, Sharma M. On-line approximation based control of uncertain nonlinear systems［C］∥Proceeding of the 2004 American Control Conference. Boston, Massachusetts: IEEE, 2004: 2557-2562.
[19]
［2］ Bezick S, Rusnak I, Gray W S. Guidance of a homing missile via nonlinear geometric control methods［J］. Journal of Guidance, Control, and Dynamics, 1995, 18(3): 441-448.
[20]
［3］ Song S H, Ha I J. A Lyapunov-like approach to performance analysis of 3-dimensional pure PNG laws［J］. IEEE Transactions on Aerospace and Electric Systems, 1994, 30(1): 238-247.
[21]
［4］ Yang C D, Chen H Y. Nonlinear robust guidance law for homing missiles［J］. Journal of Guidance, Control, and Dynamics, 1998, 21(6): 882-890.
