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

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)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1969
Accession Number
AD0691183

Tags

DTIC Thesaurus Topics

  • Altitude
  • Cathode Ray Tubes
  • Demographic Cohorts
  • Glide Slope
  • Indicators
  • Resilience

Readers

  • Aviation Safety and Air Traffic Management
  • Human-Computer Interaction (HCI).
  • Inertial Navigation Systems.