Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1987-04-29
1988-05-31
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 15033
Patent
active
047475684
ABSTRACT:
A missile flight control system includes a plurality of fins movable by actuators and a corresponding plurality of valves each of which regulates gas flow through a pair of outlets which are oppositely directed perpendicularly of the missile axis, the valve being operated by respective ones of the actuators.
REFERENCES:
patent: 3637167 (1972-01-01), Froning, Jr. et al.
patent: 4085909 (1978-04-01), East et al.
patent: 4560121 (1985-12-01), Terp
Jordan Charles T.
Lucas Industries PLC
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