Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1986-04-09
1987-12-08
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 321, F41G 700
Patent
active
047114126
ABSTRACT:
A method for homing onto a target detected forwardly laterally or sideways offset from the glide trajectory of a projectile which is equipped with a search head, with control surfaces and with horizontal glide surfaces, through the implementation of roll motion for the yaw maneuver.
REFERENCES:
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patent: 2824710 (1958-02-01), Hall
patent: 3695555 (1972-10-01), Chadwick
patent: 3946968 (1976-03-01), Stallard
patent: 4530476 (1985-07-01), Thurber, Jr. et al.
patent: 4590567 (1986-05-01), Hofmann et al.
patent: 4606514 (1986-08-01), Sundermeyer
Defense Electronics, Jun. 1984, p. 102.
Diehl GmbH & Co.
Jordan Charles T.
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