METHOD FOR SHAPING A MISSILE CONTROL SIGNAL WHEN GUIDING TO A MANEUVERING TARGET Russian patent published in 2019 - IPC F41G7/22 

FIELD: physics.

SUBSTANCE: invention relates to navigation instrumentation and can be used in guidance systems for shaping a missile control signal. Technical result is higher accuracy. For this the invention comprises, for calculating a rocket control signal when guiding to a manoeuvring target, calculating reachability areas in the form of geometric figures bounded by a part of a circular arc and a curve connecting extreme points of the arc, taking into account the characteristic points of the reachability areas of the missile and manoeuvring target, and selecting control of the missile based on the position of the most distant point of the reachability area of the manoeuvring target relative to the reachability area of the missile for the selected hypothetical impact point.

EFFECT: provided is increased accuracy of guiding the missile to a target, increased effectiveness of the use of missile armament when firing at high-speed and highly manoeuvrable targets while maintaining the computational complexity of the method compared with the closest analogue.

1 cl, 1 dwg