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:

1975-11-18

Pagination or Media Count:

5.0

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