Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1977-10-05
1980-02-19
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 1502
Patent
active
041891163
ABSTRACT:
This invention concerns a navigation system of the type utilizing proportional navigation guidance laws to guide an aerodynamically controlled body tracking a target, and particularly relates to a navigation system mechanization wherein necessary body-to-target line-of-sight rate-of-change information with respect to an inertial reference is developed implicitly, in part by using system optics and detector elements that are fixed to the guided body rather than to a body-mounted, inertially stabilized platform, to obtain stabilized guidance system tracking.
REFERENCES:
patent: 3398918 (1968-08-01), Girault
patent: 3640628 (1972-02-01), Jones
patent: 4020339 (1977-04-01), Gustafson
patent: 4021007 (1977-05-01), Coxe
Ehrich Ralph D.
Emmert Robert I.
Hamann H. Fredrick
Humphries L. Lee
Jordan Charles T.
Pitts Rolf M.
Rockwell International Corporation
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