Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1989-01-23
1990-05-29
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 15033
Patent
active
049289063
ABSTRACT:
A remote control for a rolling flying body enables that body to also perf pitching movements about its pitch axis and yawing movements about its yaw axis. For this purpose the flying body is equipped with a plurality of control nozzles distributed about the circumference of the flying body. These control nozzles or rather the fluid flow through the control nozzles is so controlled by control valves that two nozzles forming a pair are simultaneously activated for causing the desired pitching and yawing movements. The duration of the control impulse signals is determined exclusively by the rolling frequency of the flying body or missile.
REFERENCES:
patent: 3184182 (1965-05-01), May
patent: 3807660 (1974-04-01), Le Corviger et al.
patent: 3926390 (1975-12-01), Teuber et al.
patent: 4482107 (1984-11-01), Metz
patent: 4681283 (1987-07-01), Kranz
patent: 4712747 (1987-12-01), Metz et al.
Fasse W. G.
Jordan Charles T.
Kane, Jr. D. H.
Messerschmitt-Boelkow-Blohm Gesellschaft mit beschraenkter Haftu
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