Laser optical lever adjunct

Optics: measuring and testing – Angle measuring or angular axial alignment – With photodetection remote from measured angle

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356154, G01B 1126, G01C 100

Patent

active

041231686

ABSTRACT:
A system and apparatus for accurate measurement of a rocket's attitude that includes a laser source placed downrange and pointed towards the rocket with a diverging beam. The beam will be intercepted by a mirror on the rocket's ogive, and the reflected beam will then be presented on a vertical target. A detector assembly positioned behind the vertical target plane detects the centroid of the reflected energy and provides an analog output signal.

REFERENCES:
patent: 3851844 (1974-12-01), Stripling et al.
patent: 3875402 (1975-04-01), Parkin
patent: 3891323 (1975-06-01), Ryan et al.
patent: 3964695 (1976-06-01), Harris
Sweigart et al.; Optical Lever Flight Instrumentation; Report No. RT-TR-78; U.S. Army Missile Command; Oct. 1970.

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