Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1989-09-19
1991-01-08
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
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.
British Aerospace Public Limited Company
Jordan Charles T.
Lieberman Rochelle
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