MANAGEMENT SYSTEM corrected air bombs, designed to defeat radio-electronic means ENEMY

摘要

FIELD: weapons and ammunition.;SUBSTANCE: invention is designed for use in control of flight of a corrected aviation bomb (CAB) in order to destroy radio-electronic facilities (REF) of an enemy. The system comprises a passive radio engineering self-homing head (PRESHH), a carrier communication unit (CCU), a control unit (CU), two switchboards, a homing command generation unit (HCGU), an inertial navigation system (INS), a solid engine control unit (SECU), an autopilot (AP), steering drives (SD), aerodynamic control surfaces (ACS) and a solid engine (SE). The first control inputs of switchboards K₁, K₂ and the autopilot are connected with the first output of the CU, the first input of which is connected with the first output of the CCU, the second input - with the second output of the INS, and the third input - with the first output of the PRESHH. The second output of the PRESHH is connected to the second input of the switchboard K1; the third output is connected with the first input of the CCU, and the input is connected with the third output of the CU. The second output of the CU is connected to the third input of the switchboard K₁, the first output of which is connected with the input of the HCGU. The output of the HCGU is connected to the second input of the switchboard K₂, the second output of the switchboard K₁ is connected with the input of the INS. The first output of the INS is connected to the third input of the switchboard K₂, and the third output - to the second input of the SECU. The output of the SECU is connected to the SE, and the first input is connected to the fourth output of the CU. The output of the switchboard K₂ is connected to the input of the AP. At the same time the second input of the CCU is the input, and its second output - the output of the system.;EFFECT: invention provides for increased probability of REF target destruction and reduced of required CAB squad for REF destruction.;2 dwg, 1 tbl