Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1981-08-12
1985-07-23
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
89 1801, 89 1805, 244 31, F41G 722, F41F 300, F42B 1516
Patent
active
045304769
ABSTRACT:
A method and system for delivering ordnance to a target via a remotely piloted or programmable aircraft including a yaw-to-turn guidance system, a deployment and launching system and packaging for the aircraft are disclosed.
REFERENCES:
patent: 1663058 (1928-03-01), Peppin
patent: 2603434 (1952-07-01), Merrill
patent: 2824710 (1958-02-01), Hall
patent: 4202516 (1980-05-01), Benser
patent: 4296894 (1981-10-01), Schnabele et al.
Behrens Frederick A.
Hunton John H.
Thurber, Jr. Charles H.
E-Systems Inc.
Jordan Charles T.
Rogers, III L. Lawton
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