Development of Handling Quality Criteria for Aircraft with Independent Control of Six Degrees of Freedom

Abstract

A tentative flying quality criterion has been developed for aircraft with direct force controls which allow independent control over the six inertial degrees of freedom. The criterion is based on analysis of existing flight test and simulation data as well as the results of an abbreviated flight test conducted during the program. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1981
Accession Number
ADA100045

Entities

People

  • Irving L. Ashkenas
  • Robert F. Ringland
  • Roger H. Hoh
  • Samuel J. Craig
  • Thomas T. Myers

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Bandwidth
  • Birds
  • Closed Loop Systems
  • Control Surfaces
  • Control Systems
  • Control Systems Engineering
  • Dynamic Response
  • Fighter Aircraft
  • Flight Control Systems
  • Frequency
  • Simulations
  • Standards
  • Statistical Analysis
  • Transport Aircraft

Fields of Study

  • Physics

Readers

  • Aviation Science / Aeronautics.
  • Systems Analysis and Design