“…(2) u M (t) or u T (t) implies the time history of the missile's or target's normalized control input described in Eq. ( 1), and r(t) is the range between the missile and the target at time t. This kind of differential game can be solved by some numerical algorithms, such as indirect methods, the gradient-based method (Tahk et al, 1998), the bilevel programming (Ehtamo & Raivio, 2001), and co-evolutionary methods (Kim & Tahk, 2001;Choi, Ryu, Tahk, & Bang, 2004). This work employs the gradient-based method devised by Tahk et al (1998), which is a direct optimization method based on control input parameterization.…”