[1] [1] QIAN X F,LIN R X,ZHAO Y N.Flight mechanics of guided missile［M］.Beijing：Beijing Institute of Technology Press,2008.

[2] [2] ZARCHAN P.Tactical and strategic missile guidance［M］.5th ed.San Diego：American Institute of Aeronautics and Astronautics,2007.

[3] [3] ZHOU D,MU C,LING Q,et al.Optimal sliding-mode guidance of a homing-missile［J］.Chinese Journal of Aeronautics,1999,12(4):236-241.

[4] [4] ZHOU D,MU C,XU W L.Adaptive sliding-mode guidance of a homing missile［J］.Journal of Guidance,Control and Dynamics,1999,22(4)：589-594.

[5] [5] WANG Z,JIA X H,YAN J.Study on the ENDGAME sliding-mode guidance law of air-to-air missile［J］.Aero Weaponry,2005(2):3-6.

[6] [6] LI Y.Study on variable structure terminal guidance law and stability of space interception［D］.Harbin：Harbin Institute of Technology,2011.

[7] [7] YUAN L Y.Nonlinear guidance law for interception of maneuvering target［D］.Harbin：Harbin Institute of Technology,2008.