This recommended practice covers the requirements for gyroscopically stabilized Directional Indicating Systems, which will operate as a 1°/hour latitude corrected, free directional gyro or as a slaved gyro, magnetic compass with 1/2° accuracy.
DIRECTIONAL INDICATING SYSTEM (TURBINE POWERED SUBSONIC AIRCRAFT)
1991-05-01
Conference paper
English
Directional Indicating System (Turbine Powered Subsonic Aircraft)
SAE Technical Papers | 2008
Directional Indicating System (Turbine Powered Subsonic Aircraft)
SAE Technical Papers | 2020
Flilght Directors (Turbine-Powered Subsonic Aircraft)
SAE Technical Papers | 2008
TEMPERATURE INSTRUMENTS (TURBINE POWERED SUBSONIC AIRCRAFT)
SAE Technical Papers | 2008
AUTOMATIC PILOTS (Turbine Powered Subsonic Aircraft)
SAE Technical Papers | 1963