METHOD OF MISSILE REMOTE CONTROL Russian patent published in 2012 - IPC F41G7/00 

FIELD: weapons and ammunition.

SUBSTANCE: prior to launching a missile, in a missile flight time function threshold values are generated for the permissible control overload of a missile. After missile launching, in a missile flight time function the current value of available missile overload is generated, using commands of missile control in channels of pitch and hunting to their limitation, the current required overload is identified for missile aiming at a target with account of a programme value of a transfer coefficient of an open missile control circuit. The current value of available overload of a missile is compared with the current threshold value of the permissible control overload of a missile and with the current value of the permissible overload, and using comparison results, a limitation coefficient is identified, proportionately to which commands of missile control are converted in channels of pitch and hunting.

EFFECT: expansion of functional capabilities.

3 cl, 3 dwg