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

Personal Author(s):

Report Date:

1969-06-01

Pagination or Media Count:

30.0

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

Subject Categories:

  • Flight Control and Instrumentation

Distribution Statement:

APPROVED FOR PUBLIC RELEASE