METHOD OF MISSILE CONTROL Russian patent published in 2010 - IPC F42B15/01 

FIELD: weapons and ammunition.

SUBSTANCE: method of control includes missile launching at the angle to line of target sighting with further matching with it along program trajectory of launch, missile acceleration with the help of booster engine, generation of program command of missile control at the section of flight trajectory with operating engine and transmission of program command to missile. The novelty is the fact that weight function is formed online as function of linear combination of module of average transverse speed of wind and module of angular speed of target sighting line. At the moment of missile launch, value of missile launching angle, program trajectory of launch and program command of missile control are corrected proportionally to value of weight function. At the same time in inclined plane of missile control, direction of missile launch angle, direction of program trajectory of launch relative to line of target sighting and sign of program command are identified at the moment of missile launching with account of the average transverse speed of wind and angular speed of target sighting line.

EFFECT: less deviations of missile relative to line of target sighting and reduced time of missile delivery within the borders of hitting area with provision of noise immunity of target and missile sighting lines under conditions of smoke disturbance caused by own shot.

1 dwg