Accession Number : ADD002284
Title : Rate-Gyro Stabilized Platform.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C
Personal Author(s) : Woodworth,William H ; Moulton,Marc L
Report Date : 18 Nov 1975
Pagination or Media Count : 5
Abstract : The patent relates to an electronic guidance system compensation network of a rate gyro stabilized platform wherein missile stability is improved by compensating for the gimbals bearing, or coulomb, friction.
Descriptors : *Guided missile components, *Stabilized platforms, *Patents, Gimbals, Bearings, Gyro stabilizers, Electronic equipment
Subject Categories : Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE