The article deals with the mathematical model of the functioning of detonation device SAM medium range with a combined guidance ( inertial with radio + semi-active homing) . The basic mathematical relationships and algorithms generate commands Doppler semi-active radio controlled fuses . Analyzes the characteristics of the joint operation of the guidance system and detonation device.
detonation device, semi-active Doppler radio controlled fuses, trip computer, homing, radio fuse tripping area
"Matematycheskoe modelyrovanye vzrыvatelnoho ustroistva. Chast 1. Analyz zadachy modelyrovanyia radyovzrыvatelia sovremennыkh zur srednei dalnosty" ,
Science and Technology of the Air Force of Ukraine,