TEST AND EVALUATION OF DECRAB DISPLAY SYSTEM.

Abstract

A flight test evaluation, under simulated Category III conditions, was conducted on a three-axis attitude indicator. Heading error was presented on the third axis to be used in executing the decrab maneuver. The indicator was installed in a Federal Aviation Administration DC-7 aircraft and flight tests were conducted using four FAA flight test pilots. Data associated with the landing maneuver were collected and compared to similar data obtained from a previous evaluation of a decrab display. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1969
Accession Number
AD0684808

Entities

People

  • Robert H. Pursel

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Attitude Indicators
  • Display Systems
  • Indicators
  • Maneuvers
  • Test And Evaluation

Readers

  • Aviation Safety and Air Traffic Management
  • Robotics and Automation.