MATHEMATICAL MODELLING OF SAM AIRBORNE COMPUTER. ANALYSIS OF PROBLEMS OF SIMULATION SAM GUIDANCE AT THE STAGE OF SELF-HOMING
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Description: 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
Reference:
Skoryk, A.B., Olkhovykov, S.V., Zverev, A.A. and Kotenko, T.N. (2013), “Matematycheskoe modelyrovanye bortovoho vыchyslytelia ZUR. Analyz zadachy modelyrovanyia navedenyia ZUR na эtape samonavedenyia”, Science and Technology of the Air Force of Ukraine, No. 4(13), pp. 50-52.
Skoryk, A.B., Olkhovykov, S.V., Zverev, A.A. and Kotenko, T.N. (2013), “Matematycheskoe modelyrovanye bortovoho vыchyslytelia ZUR. Analyz zadachy modelyrovanyia navedenyia ZUR na эtape samonavedenyia”, Science and Technology of the Air Force of Ukraine, No. 4(13), pp. 50-52.