[1] QIAN X F,LIN R X,ZHAO Y N.Flight mechanics of guided missile[M].Beijing:Beijing Institute of Technology Press,2008.
[2] ZARCHAN P.Tactical and strategic missile guidance[M].5th ed.San Diego:American Institute of Aeronautics and Astronautics,2007.
[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] 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] 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] LI Y.Study on variable structure terminal guidance law and stability of space interception[D].Harbin:Harbin Institute of Technology,2011.
[7] YUAN L Y.Nonlinear guidance law for interception of maneuvering target[D].Harbin:Harbin Institute of Technology,2008.