[1] [1] KIM K S,JUNG B,KIM Y.Practical guidance law controlling impact angle[J].Proceedings of the Institution of Mechanical Engineers,Part G:Journal of Aerospace Engineering,2007,221(1):29-36.

[3] [3] YOON M G.Relative circular navigation guidance for three-dimensional impact angle control problem[J].Journal of Aerospace Engineering,2010,23(4):300-308.

[5] [5] RYOO C K,SHIN H S,TAHK M J.Energy optimal waypoint guidance synthesis for antiship missiles[J].IEEE Transactions on Aerospace and Electronic Systems,2010, 46(1):80-95.

[6] [6] SANG D,MIN B M,TAHK M J.Impact angle control gui-dance law using Lyapunov function and PSO method[C]//SICE Annual Conference,Kagawa University,Japan,2007:2253-2257.

[7] [7] LEE J I,JEON I S,TAHK M J.Guidance law to control impact time and angle[J].IEEE Transactions on Aerospace and Electronic Systems,2007,43(1):301-310.

[8] [8] YUN J,RYOO C K.Integrated guidance and control law with impact angle constraint[C]//The 11th International Conference on Control,Automation and Systems,Gyeonggi-do,2011:1239-1243.

[9] [9] LEE Y,RYOO C,KIM E.Optimal guidance with constraints on impact angle and terminal acceleration[C]//AIAA Guidance,Navigation and Control Conference, Austin,USA,2003.doi:10.2514/6.2003-5795.

[10] [10] JEON I S,LEE J I,TAHK M J.Guidance law to control impact time and angle[C]//International Conference on Control and Automation,Budapest,Hungary,2005,2:852-857.

[11] [11] SIOURIS G M.Missile guidance and control systems[M].New York:Springer,2004:181-207.