Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1965-12-03
1995-02-28
Lobo, Ian J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 1060
Patent
active
053930118
ABSTRACT:
Disclosed herein is a missile having a rotatable portion arranged for rotation relative to another portion of the missile which contains spacedly mounted electromagnetic coils for respectively operating first and second control member actuator mechanisms for controlling the missile.
REFERENCES:
patent: 3067681 (1962-12-01), Beman
patent: 3111088 (1963-11-01), Fisk
patent: 3154015 (1964-10-01), Muller
Carson Oliver S.
Dunn Albert J.
Lobo Ian J.
Shorts Missile Systems Limited
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