Navigation system

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Patent

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Details

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

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