• DocumentCode
    1339850
  • Title

    DGPS-based aircraft flight guidance/test system

  • Author

    Jia, Huamin ; Dou, Xiaomu ; Yuan, Jianping

  • Author_Institution
    Dept. of Astronaut. Eng., Northwestern Polytech. Univ., Xian, China
  • Volume
    11
  • Issue
    7
  • fYear
    1996
  • fDate
    7/1/1996 12:00:00 AM
  • Firstpage
    23
  • Lastpage
    26
  • Abstract
    The utilization of the GPS system for Aircraft Flight Guidance/Test (AFGT) is a research project in China. The paper describes the concepts and the technical realization of such a system, including three components: ground subsystem, on-board subsystem and data communication link using TDMA technique. The purpose of the proposed AFGT system is to calibrate and verify performance of an on-board radar. Therefore, it must meet the requirements of evaluation of radar performances in several areas: accuracy, coverage range, and others. The AFGT System´s displays are separately: a Moving Colored Digital Map on which flight trajectories, waypoints, and heights of aircrafts are clearly marked; and a Polar Coordinate Figure on which the bearings, headings, and distances of aircrafts relative to the origin of the ground control center are shown. The AFGT may monitor and guide several aircrafts flying in the pointed airspace. It support airport surface surveillance and air traffic control at the terminal area. A real-time software package RTTEST, which includes tracking display software and on-flight test software for radar evaluation, has conducted simulation with satisfactory position accuracy
  • Keywords
    Global Positioning System; air traffic control; airborne radar; aircraft control; calibration; data communication; ground support equipment; performance evaluation; telecommunication equipment testing; time division multiple access; China; GPS; Moving Colored Digital Map; Polar Coordinate Figure; RTTEST; TDMA; accuracy; air traffic control; aircraft flight guidance/test system; airport surface surveillance; coverage range; data communication link; flight trajectories; ground subsystem; heights; on-board radar; on-board subsystem; on-flight test software; radar performances; real-time software package; tracking display software; waypoints; Aerospace control; Air traffic control; Aircraft; Data communication; Displays; Global Positioning System; Performance evaluation; Radar tracking; System testing; Time division multiple access;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/62.533968
  • Filename
    533968