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  5. MATHEMATICAL MODELLING OF SAM AIRBORNE COMPUTER. THE PART 2. ANALYSIS OF PROBLEMS OF SIMULATION MANAGEMENT AT THE STAGE OF SAM INERTIAL GUIDANCE

MATHEMATICAL MODELLING OF SAM AIRBORNE COMPUTER. THE PART 2. ANALYSIS OF PROBLEMS OF SIMULATION MANAGEMENT AT THE STAGE OF SAM INERTIAL GUIDANCE

A.B. Skorik, O.V. Gavrentjuk, A.A. Skorik, A.M. Doska
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In this paper, a mathematical model of the functioning of the onboard calculator missiles with a combined guidance (inertial with radio + semi-active homing). The basic mathematical relationships and algorithms for production teams aiming missiles at the realization of inertial with radio control. The features of missile guidance in the implementation of "command-andinertial guidance method."
Keywords: modified method of proportional navigation, trip computer, command-and-inertial guidance method, the matrix of direction cosines, radiocorrection