METHOD FOR MISSILE FLIGHT CONTROL Russian patent published in 2016 - IPC B64C19/00 F42B15/01 F41G7/26 

FIELD: military equipment.

SUBSTANCE: invention relates mainly to tactical and operational-tactical guided weapon systems (URO) with ballistic (aeroballistic) and high-altitude cruise missiles. Optical-electronic correlation-extremum CN missile additionally includes a laser altimeter (LV). Functioning of CN is started at a distance from target and missile flight altitude of 1…20 km, wherein when LV receives reflected signals of underlying surface above threshold level, method comprises correlation-extreme binding to underlying surface and correction of curved missile trajectory to end of flight. If LV receives reflected signals below threshold, method comprises performing a program manoeuvre of missile in plane of firing with output on section of flat glide at altitude of 100…500 m for 0.5…15.0 km from target, correlation-extreme binding to underlying surface and correction of glide trajectory of missile, with diving final section for 0.1…2.0 km from target, up to end of flight.

EFFECT: invention widens weather range of application of missiles.

1 cl, 2 dwg