Method for reducing dispersion in gun launched projectiles

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Patent

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F42B 1000

Patent

active

053757920

ABSTRACT:
Disclosed is a method for reducing dispersion in gun launched projectiles. n axial thrust is applied to the projectile at a specific time in the yaw cycle to cancel the effect of aerodynamic jump which arises from the effect of yawing motion disturbance created by an initial disturbance.

REFERENCES:
patent: 5103735 (1992-04-01), Kaste et al.

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