Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1980-05-22
1982-07-13
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 722
Patent
active
043390978
ABSTRACT:
A target seeking head mounted in the dome of a missile comprises a gyro rotor including a mid-portion forming a convex calotte-shaped peripheral surface. The convex calotte-shaped peripheral surface is surrounded substantially concentrically by a concave calotte-shaped bearing surface stationary with respect to the missile. A small gap is formed between the two surfaces and pressurized gas is introduced into the gap to form a gas bearing centering the gyro in the center of curvature of the convex calotte-shaped peripheral surface thereof. A target seeking scanning device comprises an annular parabolic mirror formed at the mid-portion of the gyro and a plane mirror imaging a field of view located in infinity in the plane of a detector mounted stationary with respect to the missile.
REFERENCES:
patent: 3920200 (1975-11-01), Evans et al.
patent: 4004754 (1977-01-01), Cox et al.
patent: 4009848 (1977-03-01), Albert et al.
patent: 4030807 (1977-06-01), Briney
Gerlach Hans H.
Jansen Dirk
Kordulla Hans
Bodenseewerk Geratetechnik GmbH
Darbo Howard H.
Jordan Charles T.
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