In article questions of construction of mathematical model of functioning of airborne computer SAM with the combined prompting (inertial with radio correction + semiactive homing) are considered. The analysis of stages of functioning of an airborne computer in the course of prestarting preparation, start-up and rocket prompting is carried out. The basic mathematical parities and algorithms of development of commands of prompting SAM at a declination stage are considered.
a prompting contour, an airborne computer, cold start with the gas-check, a matrix directional cosines, rocket declination
"Matematycheskoe modelyrovanye bortovoho vыchyslytelia ZUR. Analyz zadachy modelyrovanyia upravlenyia ZUR s vertykalnыm startom na эtape sklonenyia" ,
Systems of Arms and Military Equipment,