Synthesis of optimum algorithms of trajectory control in the combined guidance system

Synthesis of optimum algorithms of trajectory control that allows executing high-precision intercept of low flying purposes is stated in the given paper. The analysis of control systems of a flight vehicle assumes research procedure in the set operating conditions for determination of parameters of its efficiency, as a rule, such parameters as response and stability, accuracy and sensitivity to change of conditions of application. Full-scale measurements by results of algorithms synthesis were executed on modeling of a contour of combined guidance by means of imitative model.