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  5. MATHEMATICAL MODELLING OF AIRBORNE COMPUTER SAM. THE ANALYSIS OF THE PROBLEM OF MODELLING OF CONTROL SAM WITH VERTICAL LAUNCH AT THE DECLINATION STAGE

MATHEMATICAL MODELLING OF AIRBORNE COMPUTER SAM. THE ANALYSIS OF THE PROBLEM OF MODELLING OF CONTROL SAM WITH VERTICAL LAUNCH AT THE DECLINATION STAGE

.A.B. Skorik, O.V. Gavrentjuk, A.A. Skorik, P.A. Drannik
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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.
Keywords: a prompting contour, an airborne computer, cold start with the gas-check, a matrix directional cosines, rocket declination