Course correction unit

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

Patent

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Details

102202, 102381, F42B 1518

Patent

active

049829130

ABSTRACT:
This invention relates to a course correction unit, specifically but not exclusively for use on a spin stabilized guided projectile which can produce high speed instantaneous course correction.

REFERENCES:
patent: 3011441 (1961-12-01), Gordon
patent: 3204559 (1965-09-01), Matthew
patent: 3380382 (1968-04-01), Jablansky
patent: 4384694 (1983-05-01), Watanabe et al.

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