The Maneuver Strategy Study Of Missile Target Basing On Variable Time Scale Adjoint Model Method

In this paper, guidance precision of exo-atmosphere interceptor is the focused subject. Basing on the theory of zero-effect miss distance, dynamics models of exo-atmosphere interceptor and it's aimed missile are developed, and variable time scale varied adjoin model of interceptor guidance system is deduced. The interceptor miss distance that arouse by missile target maneuver direction, amplitude, interceptor initial head error and angle velocity measurement error of the seeker is simulated and analyzed in detail. At the end of the paper, the effective maneuver strategy for max interception miss distance of the missile target is presented.