05.1 - Flight Dynamics and Control (Control & Modelling)
CLOSED-FORM COOPERATIVE GUIDANCE LAW FOR TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINTS
D. Leeš, J.-H. Kim, Agency for Defense Development, South Korea; H.-L. Choiš; šKAIST, South Korea
In this paper, we consider cooperative guidance problems of two missiles. The two missiles cooperate to optimize a coupled objective of control effort cost. A coupled constraint on terminal velocity is incorporated so that their vertical components sum to zero for maximum survivability. The proposed law can be used in situation under formidable defensive system to accomplish the mission.