This document describes the design of the Automatic Tracking and Control System that will be used with a Glide Slope and Localizer Scale Model ILS facilities. The design approach uses a positive drive system to control trolley height as a function of carriage displacement from threshold and glide path angle. A carriage and mast assembly simulating an aircraft on its final approach was designed and built. A digital servo system for the accurate positioning of the simulated aircraft receiving antenna was developed. (Author)

  • Corporate Authors:

    Airborne Instruments Laboratory

    Cutler-Hammer, Incorporated, Commac Road
    Deer Park, NY  United States  11729
  • Authors:
    • Palatnick, A S
  • Publication Date: 1975-7

Media Info

  • Pagination: 34 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00093529
  • Record Type: Publication
  • Source Agency: National Technical Information Service
  • Report/Paper Numbers: AIL-FGS-A414-3 Intrm Rpt., FAA-RD-75-203
  • Contract Numbers: DOT-FA74WA-3345
  • Files: NTIS
  • Created Date: Jan 21 1976 12:00AM