Paper summarizes progress from direct reading compasses to monitored gyroscopes and concentrates on unique problems in aircraft where space limitations, reliability, and operation at all altitudes are important; it indicates how azimuth indicators and auto pilot controls close to ideal are obtainable by use of special features including novel "non-tumbling" mechanism and electromagnetic type of gimbal adjusting device. (Trans)
Improved azimuth indicating system for aircraft
Elec Eng
Electrical Engineering ; 65 , n 12
1946
7 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Indicating System for Aircraft
NTIS | 1971
|SAE Technical Papers | 2015
SAE Technical Papers | 1991
SAE Technical Papers | 2004
Design of an improved azimuth reference system
AIAA | 1975
|