Mathematical Analysis of Stage-separation Regulations of Missile

This paper aiming at the attitude movement equations of missile,deduced the analytic results based on rational assumptions.The conclusion were proved in conformance with the traditional digital simulation: swing angle and swing angle velocity were turning in the form of sinusoidal periodical movements,while the periodicity was influenced by rolling angle velocity,product of inertia and the swing by moment disturbances,product of inertia,either.