COMBINED CONTROL SYSTEM OF ADJUSTABLE AIRCRAFT BOMB Russian patent published in 2013 - IPC F42B15/01 

FIELD: weapons and ammunition.

SUBSTANCE: invention is designed for use to control flight of an adjustable aircraft bomb (AAB) when inflicting blows at stationary (ground and above-water) facilities of an enemy with bombs equipped with blast warheads under conditions of radioelectronic countermeasures of the enemy. The system comprises the following: a reception indicator of satellite navigation systems (SNS), a correction device (CD), an inertial navigation system (INS), a unit of communication with a carrier (CCU), a control unit (CU), two switching devices (SD), satellite homing command generation units (SHCGU), inertial homing command generation units (IHCGU) and inertial homing and correction command generation units (IHCCGU). There are the following serially connected components: an autopilot (AP), steering linkages with a turbogenerator source of power supply (SL) and aerodynamic control surfaces (ACS). The AAB control system provides for bomb homing at a target using three homing channels - satellite, inertial and inertial-corrected according to data of the satellite channel.

EFFECT: higher probability of target destruction under conditions of electronic suppression of AAB satellite homing by an enemy.

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