[1] [1] ZHOU H R.Maneuvering target tracking［M］.Beijing:National Defence Industry Press 1991.

[2] [2] JI C X XU J H CHEN K.Development of mulitiple-model dlgorithm for tracking maneuvering target［J］.System Enginneering and Electronics 2003 25(7):882-885.

[3] [3] SUN S B SONG J M ZHANG J.Target tracking algorithm of super-low altitude interceptors based on UKF-IMM［J］.Systems Engineering and Electronics 2009 31(10):2367-2371.

[4] [4] LIN L KIRUBARAJAN T BAR-SHALOM Y.Pursuer identification and time-to-go estimation using passive measurements from an evader［J］.IEEE Transactions on Aerospace and Electronic Systems 2005,41(1):190-204.

[5] [5] SHI Z K.Computational method for optimal estimation［M］.Beijing:Science Press 2001.

[6] [6] ZHOU D.New guidance law for homing missile［M］.Beijing:National Defense Industry Press 2002.

[7] [7] Qian X F LIN R X ZHAO Y N.Missile flight aerodynamics［M］.Beijing:Beijing Institute of Technology Press 2000.

[8] [8] LEI H M.Theory of guidance and control for missile［M］.Beijing:National Defense Industry Press 2006.

[9] [9] HE B ZHANG J F.Technical research of active missile approach warning equipment［J］.Electronic Information Warfare Technology 2008 23(5):39-42.

[10] [10] LIANG Y PAN Q YANG F et al.The modern estimation theory and application of complex system［M］.Beijing:Science Press 2009.

[11] [11] CAI J S.The system identification of flight vehicle［M］.Beijing:China Astronautic Publishing House 1995.

[12] [12] SHINAR J GUELMAN M SILBERMAN G et al.On optimal missile avoidance-a comparison between optimal control and differential game solutions［C］//ICCON89 IEEE International Conference on Control and Applications 1989:453-459.