[4] GAMELL P.Guided weapon control system[M].Beijing:Beijing Institute of Technology Press,2003:297-364.

[5] KIM T H,LEE J I,TAHK M J.Time-to-go polynomial guidance laws with terminal impact angle/acceleration constraints[C]//Preprints of the 18th IFAC World Congress,Milano,Italy,2011:3915-3919.

[6] JEON I S,LEE J I,TAHK M J.Homing guidance law for cooperative attack of multiple missiles[J].Journal of Guidance,Control and Dynamics,2010,33(1):275-280.

[7] ZHANG Y A,MA G X.A biased PNG law with impact time constraint for antiship missiles[C]//Chinese Gui-dance,Navigation and Control Conference,Beijing,China,2012:874-878.

[8] SHIN H S,CHO H,TSOURDOS A.Time-to-go estimation using guidance command history[C]//Preprints of the 18th IFAC World Congress,Milano,Italy,2011:5531-5536.