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