Synthesis of control command for single-channel flying equipment by pulse width - amplitude modulation method

Abstract

 The article examines the method of synthesizing control commands of single-channel flying equipment (TBBMK) with infrared homing heads currently in use; These methods require the rudder angle to be able to change from the maximum negative value to the maximum positive value continuously or in steps. Through analyzing the mathematical model describing the flight dynamics of TBBMK based on the assumption of actual flight conditions, the authors propose to control TBBMK according to the pulse width - amplitude modulation (PWAM) method.