METHOD FOR MISSILE CONTROL Russian patent published in 2006 - IPC F42B15/01 

FIELD: rocketry, applicable in armament complexes of telecontrolled missiles.

SUBSTANCE: the method includes a missile launch at angle to the target sighting line, acceleration of the missile with the aid of the booster engine and formation of a program control command for ejection of the missile to the target sighting line. The novelty in the control method is in the fact that the direction of the missile launching angle in the direction of the cross-stream component of wind is formed, and the value of launching angle φ₀ is determined from the first mathematic expression, and from the launching moment the missile in the boost trajectory is turned in the direction of the cross-stream component of wind with the aid of the missile control surfaces, their deflection angle is formed proportionally to the program command determined according to the second mathematic expression.

EFFECT: reduced missile dispersion and enhanced accuracy of its injection to the target sighting line at a cross wind.

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