MATHEMATICAL MODELLING OF SAM AIRBORNE COMPUTER. ANALYSIS OF PROBLEMS OF SIMULATION SAM GUIDANCE AT THE STAGE OF SELF-HOMING
A.B. Skoryk, S.V. Olkhovikov, A.A. Zverev, T.M. Kotenko
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The article deals with a mathematical model of the on-board calculator SAM combined guidance (inertial with radio + semi-active homing). The basic mathematical relationships and the development of algorithms for production teams aiming missiles at the realization of self-homing. The features of the construction and operation of a complex measuring instrument.
Keywords: modified method of proportional navigation, trip computer, a complex measuring instrument
