Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1994-03-31
1994-12-27
Pihulic, Daniel T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
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.
Elbaum Saul
Goldberg Edward
Pihulic Daniel T.
Sachs Michael C.
The United States of America as represented by the Secretary of
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