Accession Number : AD0691183

Title :   ATTITUDE DIRECTOR INDICATOR SYSTEM FOR FAA ALL-WEATHER LANDING SYSTEM.

Descriptive Note : Final rept.

Corporate Author : KAISER AEROSPACE AND ELECTRONICS CORP PALO ALTO CALIF

Report Date : 01 JUN 1969

Pagination or Media Count : 30

Abstract : The attitude director indicator system utilizes cathode-ray tube image generation techniques to provide an attitude-director display with a high degree of flexibility. The display includes roll and pitch attitude, roll, pitch and yaw command, glide slope deviation, crab angle and radar altitude, and indications of failures. (Author)

Descriptors :   (*ATTITUDE INDICATORS, *ALL WEATHER AVIATION), (*AIRCRAFT LANDINGS, ATTITUDE INDICATORS), INSTRUMENT LANDINGS, DISPLAY SYSTEMS, ROLL, PITCH(MOTION), YAW, FLIGHT PATHS, ELECTRONIC EQUIPMENT

Subject Categories : Flight Control and Instrumentation

Distribution Statement : APPROVED FOR PUBLIC RELEASE